Text Books - upes.ac.in · Web viewOrigin of X-rays, Continuous X-ray Spectra, Production of Characteristic X-Ray spectra, Moseley’s law, ... Mahajan S. (2009) Modern Physics,

UNIVERSITY OF PETROLEUM & ENERGY STUDIES

(ISO 9001:2008 Certified)

B.TECH

(AEROSPACE ENGINEERING)

w.e.f. 2017

B.Tech. Aerospace Engineering 2017SEMESTER I

SEMESTER II

Subject Code Subject Credits


MATH 1001 Mathematics I 4 MATH 1004 Mathematics II 4PHYS 1001 Physics I 4 PHYS 1004 Physics II 4HBOC 1001 Design Thinking 4 COMM 1001 English Communication 4HSFS 1001 Environmental Studies 3 MECH 1001 Engineering Graphics 2MECH 1002 Engineering Mechanics 3 ECEG 1001 Basic Electrical and Electronics 3MEPD 1001 Workshop Technology 2 CSEG 1001 Computer Programming 3CHEM 1001 Chemistry 4

PRACTICAL

PRACTICAL

PHYS 1101 Physics Lab I 1 PHYS 1104 Physics Lab II 1MEPD 1101 Engineering Workshop Lab 1 ECEG 1101 Electrical and Electronics Lab 1CHEM 1101 Chemistry Lab 1 CSEG 1101 Computer Programming Lab 1

TOTAL 27 TOTAL 23SEMESTER III

SEMESTER IV



MATH 2001 Mathematics III 4 MECH 3001 Design of Machine Elements 4MECH 2012 Strength of Materials 4 ASEG 2002 Aerodynamics I 4MECH 2002 Applied Fluid Mechanics 4 ASEG 2003 Propulsion I 4

MEPD 2002 Thermodynamics & Heat Engines 4 CHCE 2001 Heat Transfer Processes 3

MECH 2013 Theory of Machine 3 Open Elective I 3

ASEG 2001 Introduction to Aerospace & Avionics Engineering

3Open Elective II 3

LNPS 1013 Venture Ideation 2PRACTICAL

PRACTICAL

MECH 2102 Applied Fluid Mechanics Lab 1 MECH 2101 Material Testing Lab 1

TOTAL 23 TOTAL 24SEMESTER V

SEMESTER VI



ASEG 3001 Flight Mechanics I 4 ASEG 3004 Propulsion II 4ASEG 3002 Aircraft Structures 4 MATH 2002 Applied Numerical Methods 4ASEG 3003 Aerodynamics II 4 MECH 3012 Introduction to Vibration 4

Open Elective III 3 Program Elective II 3Program Elective I 3

PRACTICAL

PRACTICAL

PROJ 3101 Minor Project I 3 ASEG 3102 Aircraft Structure lab 1ASEG 3104 Propulsion Lab 1

ASEG 3103 Aerodynamics lab 1 INDT 3101 Industrial Visit 1PROJ 3102 Minor Project II 3

TOTAL 22 TOTAL 21

Program Elective I Program Elective II

ASEG 3005 Aircraft Materials ASEG 3007 Theory of Plates

ASEG 3006Aircraft Systems and Maintenance ASEG 3008 Supersonic Aerodynamics

SEMESTER VII

SEMESTER VIII



ASEG 4001 Flight Mechanics II 4 ASEG 4004 Aircraft design 4ASEG 4002 Computational Fluid Dynamics 4 Program elective IV 3ASEG 4003 Finite element Methods 4 Program elective V 3

Program Elective III 3PRACTICAL

PRACTICAL

ASEG 4101 Aero Modelling & Fabrication lab 1 PROJ 4102 Major Project II 8

VIVA 4101 Comprehensive Viva 1PROJ 4101 Major Project I 4SIIB 4101 Summer Internship 2

TOTAL 23 TOTAL 18

Program Elective III Program Elective IV

ASEG 4006 Orbital Mechanics ASEG 4008Space Science & Space Environment

ASEG 4007 Helicopter engineering ASEG 4009 Composite materialsProgram Elective V

ASEG 4010 Aero-ElasticityASEG 4011 Rocket propulsion

Total Credits of B.Tech. Aerospace Engineering 2017 181

SEMESTER I SEMESTER I

PROGRAM OUTCOMES (POs):

PO1. Engineering knowledge: Apply the knowledge of mathematics, science, engineering

fundamentals, and an engineering specialization to the solution of complex engineering

problems.

PO2. Problem analysis: Identify, formulate, review research literature, and analyze complex

engineering problems reaching substantiated conclusions using first principles of mathematics,

natural sciences, and engineering sciences.

PO3. Design/development of solutions: Design solutions for complex engineering problems

and design system components or processes that meet the specified needs with appropriate

consideration for the public health and safety, and the cultural, societal, and environmental

considerations.

PO4. Conduct investigations of complex problems: Use research-based knowledge and

research methods including design of experiments, analysis and interpretation of data, and

synthesis of the information to provide valid conclusions.

PO5. Modern tool usage: Create, select, and apply appropriate techniques, resources, and

modern engineering and IT tools including prediction and modeling to complex engineering

activities with an understanding of the limitations.

PO6. The engineer and society: Apply reasoning informed by the contextual knowledge to

assess societal, health, safety, legal and cultural issues and the consequent responsibilities

relevant to the professional engineering practice.

PO7. Environment and sustainability: Understand the impact of the professional engineering

solutions in societal and environmental contexts, demonstrate the knowledge of, and need for

sustainable development.

PO8. Ethics: Apply ethical principles and commit to professional ethics, responsibilities, and

norms of the engineering practice.

PO9. Individual and Teamwork: Function effectively as an individual, and as a member or

leader in diverse teams, and in multidisciplinary settings.

PO10. Communication: Communicate effectively on complex engineering activities with the

engineering community and with society, such as, being able to comprehend and write effective

reports and design documentation, make effective presentations, and give and receive clear

instructions.

PO11. Project management and finance: Demonstrate knowledge and understanding of the

engineering and management principles and apply these to one’s own work, as a member and

leader in a team, to manage projects and in multidisciplinary environments.

PO12. Life-long learning: Recognize the need for, and have the preparation and ability to

engage in independent and life-long learning in the broadest context of technological change.

PROGRAM SPECIFC OUTCOMES (PSOs):

PSO1: Apply the principles of core engineering fundamentals of Aerodynamics, Propulsion, Structures, Flight Mechanics and space science in Aerospace Engineering.

PSO2: Have skills to conceive, design, implement and operate aerospace systems

SEMESTER I

Course Code

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

MATH 1001

3 2 0 0 2 0 0 0 0 0 0 0 0 0

PHYS 1001 3 2 0 0 0 0 0 0 0 0 0 0 0 0HBO1001 0 0 3 2 2 1 2 1 1 1 2 3 0 1HSFS 1001 1.5 2.5 2 0 0 1.8 2.3 0 0 0 1 0 0 0MECH 1002

3 3 2 0 3 0 0 2 0 0 2 0 0 1

MEPD 1001

2.33

0 1.67

0 1.67

2.3 2 0 0 1.33 2 3 0 0

CHEM 1001

3 2 0 0 0 0 1 0 0 0 0 0 0 0

SEMESTER II

Course Code

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

MATH 1004

3 2 0 0 2 0 0 0 0 0 0 0 0 0

PHYS-1004 3 2 0 0 0 0 0 0 0 0 0 0 0 0COMM1001

0 0 0 0 0 0 0 0 1 3 0 2 0 0

MECH1001 3 3 3 2 3 0 0 0 0 2 0 0 0 0ECEG 1001 3 3 2 1 1 0 0 0 0 0 0 1 0 0CSEG 1001 3 2 1 0 1 0 0 0 0 0 1 0 0 0

SEMESTER III

Course Code

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

MATH 2001

3 2 0 0 2 0 0 0 0 0 0 0 0 0

MECH 2012

3 2.75

1.6 2 2 0 2 0 0 0 0 1 2 1

MECH 2002

2.8 0 3 0 3 0 0 0 0 2 2 1.5 2 1.7

MEPD 2002

3 2.75

1.67

2 2 0 2 0 0 0 0 1 1.67 0

MECH 2013

3 3 0 0 0 0 0 0 0 1 1 0 0 0

ASEG 2001 1 1 1 0 0 1 0 0 0 0 0 1 2 1SEMESTER IV

Course Code

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

MECH 3001

3 3 2.6 1.8 1.8 0 0 0 0 2.6 2.6 1 0 2.8

ASEG 2002 3 2.4 0 1.4 0 0 0 0 0 0 0 1 3 0ASEG 2003 3 2.5 2.3

32.33

0 0 0 0 0 0 0 0 3 1.5

CHCE 2001 2.6 2.4 1.7 1 0 0 0 0 0 2 0 0 0 0LNPS 1013 0 0 2 3 0 2 0 0 1 1 2 0 0 0

SEMESTER V

Course Code

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

ASEG 3001 3 3 2 1.4 0 0 1 0 1 0 0 0 3 1ASEG 3002 3 2.8 1.8 2.8 2 0 0 0 0 0 0 0 3 1ASEG 3003 2.6 0.4 0 0.6 0.5 0 0 0 0 0 0 1.6 3 2.4ASEG 3005 2 1 1 0 0 0 0 0 0 0 0 0 2 0ASEG-3006 2 1.7

51 1.6

71.75

0 1 0 0 0 0 1 2.25 1

SEMESTER VICourse Code

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

ASEG 3004 2.8 2.8 2 0 1 0 2 0 0 0 0 0 2.8 1.67MATH 2002

3 2 0 0 2 0 0 0 0 1 0 0 0 0

MECH 3012

2.75

1.25

1 0 0 0 0 0 0 0 0 2.25 2.25 1.5

ASEG 3007 3 2.25

1 1.75

0 0 0 0 0 0 0 0 3 1

ASEG 3008 3 2.67

1.83

1.6 0 0 0 0 0 0 0 0 3 1.8

SEMESTER VII

Course Code

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

ASEG 4001 2 1.8 1 2 0 1 0 0 0 0 0 2 3 2ASEG 4002 2.7 1 0 1 2.5 0 0 0 1 0 0 2 3 2ASEG4003 2.2 2.5 1.5 3 1.3

30 0 0 0 0 0 2 1.5 1

ASEG 4006 1.67

2 1 2 2 0 1 0 0 1 0 1.33 1.33 1

ASEG 4007 2 1.6 1.8 1.6 0 1 0 0 0 0 0 1 3 1.6SEMESTER VIII

Course Code

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

ASEG 4004 2 1.8 2.6 1.4 1.6 1 1 0 0 0 2 1.6 3 3ASEG 4008 1 1.5 0 1.7

51.75

1 1.8 0 0 2 0 1.25 1.5 0

ASEG 4009 2.2 2 2 0 0 0 0 0 0 0 0 0 2.2 1ASEG 4010 3 2.8 2.2 2.8 0 0 0 0 0 0 0 0 3 1.75ASEG-4011 2.6 1.8 2 2.5

22 0 1 0 2 0 0 2 2.8 2.2

NOTE:- All the sections are compulsory. The notations have their usual meanings. Make suitable

assumptions while answering the questions. Assume suitable data if missing.

SECTION-A (4 X 5 = 20 MARKS)

Q.1 What is shear center? What are the properties of the shear center? Explain the importance of shear center in aircraft structure.

CO2

Q.2 An unsymmetrical T cross-section having the cross-sectional properties are Ixx = 1.09 x 106 mm4, Iyy = 1.31 x 106 mm4, Ixy = 0.34 x 106 mm4

respectively, and is subjected to a bending moment of 1500Nm in a vertical plane. Calculate the position of neutral axis.

CO4

Q.3 Calculate the cross-sectional properties (Ixx, Iyy and Ixy) of the section as shown in figure-1.

CO1

Q.4 The figure-2 shows a cross section of an aluminum rubber tab. Determine the Maximum value of the torque T can resists by the panels so that the maximum shearing stress in any of the member cannot exceed 90 MPa. Take Eal = 70 Gpa, Gal = 26 Gpa. Assume t = 5mm same for all members

CO4

Figure-1 Figure-2

UNIVERSITY OF PETROLEUM & ENERGY STUDIESDEHRADUN

End Semester Examination – Model Question Paper

Program/course: B.Tech Aerospace Engineering Semester – V Subject: Aircraft Structures Max. Marks : 100Code : ASEG 3002 Duration : 3 HrsNo. of page/s: 03

SECTION – B (4 X 10 = 40 MARKS)

Q.5 For the uniform thickness open section as shown in the Figure-3. Find the location of the shear center. Assume constant thickness t is same for all the members.

CO5

Q.6 Calculate the angle of twist at the free end of the cantilevered idealized box beam as shown in Figure-4. The values of the boom areas and the wall thickness are shown in Figure-4.

CO5

Q.7 Calculate the displacement of point C of the truss as shown in Figure-4, in the direction of the incline using Energy method or Matrix method.

CO6

Q.8 Determine the location of shear center of the idealized open section as shown in figure-5, is subjected a vertical shear force of 10 kN through the shear center.

CO4

Figure-3 Figure-4

Figure – 4 Figure-5

SECTION – C (2 X 20 MARKS)

Q.9 Calculate the maximum compressive and maximum tensile values of the axial stress at the built-in end of the cantilever beam as shown in Figure-6. The detail of the hollow section and the loads on the beam are shown in Figure-6.

CO1, CO2

Q.10 A thin walled square section has a small slit at the midpoint of the vertical wall as shown in Figure-7. Find the maximum shear stress if the section transmits a load P applied as shown in Figure below. Compare that to the maximum shear stress if there were no slit. The walls are effective in bending as well as in shear.

CO4

OrThe three boom idealized section as shown in Figure-8 is subjected to following loads: Mx = 1 KN-m; My = 4 KN-m; T = 2 KN-m clockwise; and the shear forces of 6KN and 8KN applied as shown. Find the boom stresses and the shear flows distribution. Also find the rate of twist. Given G = 40GPa, B1 = B2 = 200 mm2, B3 = 300 mm2. t = 2 mm for all webs.

CO5

Figure-6

Figure – 7 Figure-8

SEMESTER I

MATH 1001 MATHEMATICS I L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure 12th level Mathematics

Co-requisites --

COURSE OBJECTIVES1. To enable students to apply matrix theory in engineering problems. 2. To help the students understand the technique to expand functions of one

and two variables and to trace the curves. 3. To develop students’ skills to calculate the area, volume, mass, centroid and

moments of inertia of plane and solid regions using the principles of multiple integration.

4. To enable students to compute Fourier series of periodic functions.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Find the Eigen values, Eigen vectors and solution of system of linear algebraic equations using the techniques of matrix theory.CO2. Apply the principles of differentiation to the problems related to extreme values, curve tracing and expansion of functions.CO3. Calculate the area, volume, mass, centroid and moment of inertia of plane and solid regions using the principles of multiple integration.CO4. Represent periodic functions of a single variable as Fourier series.

CATALOG DESCRIPTIONMathematics is a necessary subject to a clear and complete understanding of virtually all phenomena. It helps us to develop logical thinking and also to find the right way to solve problems. This course covers Matrix theory, Differential calculus, Multiple integrals and Fourier series. This course is designed in such a way that it enables the students to cope confidently with the mathematics needed in their future subjects and the curriculum aims at developing student’s ability to conceptualize, reason and to use mathematics to formulate and solve problems in their core subjects.

Course Content UNIT I: MATRICES 9 LECTURE

HOURS

Introduction: Revision of Prerequisites, Elementary Row and Column Transformations(Reduction of a Matrices into Echelon and Normal form), Linear Dependence of Columns and Rows, Rank of a Matrix, Consistency of System of Linear Equations and its Solution, Characteristic Equation, Eigen values and Eigenvectors, Applications of Cayley-Hamilton Theorem, Diagonalisation.

UNIT II: DIFFERENTIAL CALCULUS 16 LECTURE HOURSHigher order derivatives, Successive Differentiation, Leibnitz Theorem, Maclaurin's and Taylor’s Theorem, Expansion of Functions of one variable, Partial Differentiation, Euler’s Theorem and its Applications, Jacobian, Expansion of Functions of two variables, Extrema of Functions of two variables, Asymptotes, Curve Tracing (Cartesian, Polar & Parametric Curves).

UNIT III: MULTIPLE INTEGRALS 10 LECTURE HOURSDouble and Triple Integrals, Change of Order of Integration, Change of Variable, Beta and Gamma Functions, Applications of I (Area, Volume, Center of Gravity & Moment of Inertia).

UNIT IV: FOURIER SERIES 7 LECTURE HOURSIntroduction to Periodic Functions, Fourier Series Expansion of Functions of Period 2π, Change of Interval, Half Range Sine and Cosine series.

Text Books1. R. K. Jain and S. R. K. Iyengar, Advanced Engineering Mathematics, Narosa Publications.

ISBN: 9788184875607.2. E. Kreyszig, Advanced Engineering Mathematics, Wiley Publications. ISBN: 9788126531356. 3. B. V. Ramana, Higher Engineering Mathematics, Tata McGraw Hill. ISBN: 9780071070089.

Reference Books1. M. D. Greenberg, Advanced Engineering Mathematics, Pearson Education, India.

ISBN: 9788177585469.2. S. Narayan, Differential Calculus, Shyamlal Charitable Trust, New Delhi. ISBN: 9788121904711.3. N. Piskunov, Differential and Integral Calculus, CBS, New Delhi, India. ISBN: 8123904932.4. J. Stewart, Essential Calculus: Early Transcendentals, Cengage Learning India Pvt. Ltd.

ISBN: 8131503453.5. D. G. Zill, Advanced Engineering Mathematics, Jones & Bartlett, India. ISBN: 9789384323271.

Modes of Evaluation: Class tests/Assignment/Tutorial Assessment/Written ExaminationExamination Scheme:

Components Tutorial/Faculty Class Tests MSE ESE

http://www.flipkart.com/author/n-piskunov

Assessment

Weightage (%) 15 15 20 50

Relationship between the Program Outcomes (POs), Program Specific Outcomes and Course Outcomes (COs)

CO/PO PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 PO12 PSO1 PSO2CO1 3 2 0 0 2 0 0 0 0 0 0 0 0 0CO2 3 2 0 0 2 0 0 0 0 0 0 0 0 0CO3 3 2 0 0 2 0 0 0 0 0 0 0 0 0CO4 3 2 0 0 2 0 0 0 0 0 0 0 0 0Average 3 2 0 0 2 0 0 0 0 0 0 0 0 0

1. WEAK 2. MODERATE 3. STRONG

PHYS 1001 Physics I L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure 12th level PhysicsCo-requisites 12th level Mathematics

COURSE OBJECTIVES1. To help students to develop an insight of optics with deep understanding of

LASERs and Holography, which have revolutionized modern technology significantly.

2. To enable students develop an understanding of crystal structure and X-ray diffraction, which has widespread applications in material analysis/characterization and instrumentation.

3. To give the students perspective of electromagnetic theory keeping in view, its widespread applications in signal transmission and electric circuit theory. This in itself is a prerequisite for solving many core-engineering problems.

4. To enable students in grasping concepts related to acoustics and vibrations with applications in building and machine design.

COURSE OUTCOMES On completion of this course, the students will be able toCO1: To understand the physics of crystals, working of LASER and optical fiber propagation mechanism electromagnetic waves and ultrasonic waves.CO2: To calculate various physical parameters related to crystals, electromagnetic and ultrasonic waves and working of LASER and optical fiber.CO3: To apply the concepts of electromagnetic and ultrasonic waves; crystal structure in understanding of materials and LASER in fiber optics and holography; CO4: To analyze the behavior of electromagnetic waves and effect of medium, application of ultrasonic waves in Acoustic of buildings and properties of LASER in optical fibers.

CATALOG DESCRIPTIONPhysics is the backbone of every engineering stream. It is helpful in investigating the mysteries of nature and how this understanding facilitates the explanation of all the physical processes, which affect us in almost every possible manner. The Physics I curriculum provides direct coherence of concepts and applications which adhere to the need of understanding engineering in a generic and dynamic manner. The course plan starts with an introduction to optics to develop an understanding of

optics, which helps to understand subsequent topics related to the working of Lasers, Holography, Fiber optics communication system and optical instrumentation. These topics form the backbone of communication technologies employed nowadays. The understanding of crystal structure and X-ray diffraction is a prerequisite for material analysis/characterization, which is very important in probing physical properties of elements and compounds. Thereafter an understanding of electromagnetic theory is emphasized, which will be helpful in conceptualizing the signal communication techniques and it forms the basis of electric signal theory. This is indeed a prerequisite for any technology under development. At the end, the topic on acoustics will help the students foray into the Science of sound & vibrations. This topic will develop an understanding of building and machine design by improving their acoustic properties.

Course Content UNIT I: 12

LECTURE HOURSLaser and Fiber Optics: Introduction to wave optics: Interference, Diffraction and Polarization Laser: Spontaneous and Stimulated emission of radiation, Einstein’s A and B coefficients, Population inversion & types of pumping, Properties of laser beam, Construction & working of Ruby and Helium-Neon laser and their application, Elementary idea of holography; construction and reconstruction of hologram Optical Fiber: Fundamental ideas about optical fiber, Types of fibers, Acceptance angle and cone, Numerical aperture, Propagation mechanism and communication in optical fiber

UNIT II: 10 LECTURE HOURSCrystal Structure and X-Rays: Unit cell, Bravais Lattices, crystallographic planes, Miller indices, inter planar distance in cubic lattice, Calculation of number of atoms per unit cell, atomic radius, coordination number, packing factor for SC, BCC, FCC and HCP structures.Origin of X-rays, Continuous X-ray Spectra, Production of Characteristic X-Ray spectra, Moseley’s law, X-ray diffraction and its applications in crystallography

UNIT III: 8 LECTURE HOURS

Electromagnetic waves and propagation: Displacement current, Maxwell’s correction in Ampere’s law, Maxwell’s Equations (Integral and Differential Forms) and Equation of continuity, EM-Wave equation and its propagation characteristics in free space and in conducting media, Poynting theorem and Poynting vectors.

UNIT IV: 10 LECTURE HOURSAcoustic and ultrasonic waves: Characteristics of sound, Classification of sound, Weber-Fechner Law, Sabine’s reverberation formula: rate of growth and decay of sound energy, Absorption coefficient and its determination, factors affecting acoustic of buildings and their remedies.Production of ultrasonic waves by magnetostriction and piezoelectric methods: acoustic grating, Detection of ultrasonic waves, properties of ultrasonic waves, Non Destructive Testing: pulse echo system through transmission and reflection modes: Applications

Text Books1. Vasudeva A.S. (2013) Modern Engineering Physics, S. Chand. ISBN: 978-81219175752. Malik H.K., Singh A.K. (2010) Engineering Physics, Tata Mc Graw Hill Education Pvt Ltd. ISBN:

978-00706715393. Sadiku M.N.O. (2008) Elements of Electromagnets, Oxford University Press. ISBN: 978-0195692075

Reference Books1. Griffiths D.J. (2012) Introduction to Electrodynamics, PHI Learning Pvt. Ltd. ISBN: 978-

8120347762. 2. Kittel C. (2012) Introduction to Solid State Physics, Willey. ISBN: 978-8126535187.3. Ghatak A. (2012) Optics, McGraw Hill Education. ISBN: 978-1259004346.4. Beiser A., Mahajan S. (2009) Modern Physics, McGraw Hill Education. ISBN: 978-00701515505. Pillai S.O. (2015) Solid State Physics, New Age International Pvt Ltd. ISBN: 978-8122436976

Modes of Evaluation: Quiz/Assignment/ presentation/ extempore/ Written ExaminationExamination Scheme:

Components CCT Tutorials/Assignments MSE ESEWeightage (%) 15 15 20 50


PO/CO

PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 PO12 PSO1 PSO2

CO13 0 0 0 0 0 0 0 0 0 0 0 0 0

CO23 2 0 0 0 0 0 0 0 0 0 0 0 0

CO33 2 0 0 0 0 0 0 0 0 0 0 0 0

CO43 2 0 0 0 0 0 0 0 0 0 0 0 0

Average

3 2 0 0 0 0 0 0 0 0 0 0 0 0


HBO1001 DESIGN THINKING L T P CVersion 1.0 4 0 0 4Pre-requisites/Exposure Knowledge of analyzing society problems and product usage

problems and a zeal to improve the current situation , in addition to knowing to using laptop/computers, internet, social media interaction, file sharing and uploading, email and communication etiquettes.

Co-requisites --

COURSE OBJECTIVES1. Increase ability to communicate with people.2. Enhance knowledge, imagination and be more assertive on opinions on problems in society.3. Learn basics of research, data collection, analysis, brainstorming to find solutions to issues.4. Apply Design Thinking methodologies to problems in field of study and other areas as well.5. Prepare the student for future Engineering positions with scope of understanding dynamics of working between Inter departments of a typical OEM.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Examine design thinking concepts and principlesCO2. Practice the methods, processes, and tools of design thinkingCO3. Apply the Design Thinking approach and model to real world scenariosCO4. Analyze the role of primary and secondary research in the discovery stage of design thinking.

CATALOG DESCRIPTIONDesign thinking course is a completely online course offered to the first year B.Tech across all streams. The course is offered by Laureate Design University for UPES Students along with Domus Academy Milan and New School of Architecture & Design, San Diego. The Design Thinking Model introduced in this course helps us to understand the steps followed in the process of designing a solution to a problem. The online course has 8 modules to be completed in 8 weeks. Hence each module is allotted a week for understanding and assignment submissions.

Course Content UNIT 1: WHAT IS DESIGN THINKING 6

LECTURE HOURSDesigners seek to transform problems into opportunities. Through collaboration, teamwork, and creativity, they investigate user needs and desires on the way to developing human0centered products and/or services. This approach is at the very heart of design thinking.

UNIT II: THE DESIGN THINKING MODEL 06 LECTURE HOURSA tool that helps guide you along a design thinking path. The model does this by providing a series of activities that that will help you effectively design a product, service or solution to a user’s need. The model presents the approach as a process, allowing us to look at each step – or phase – along the journey to the development of a final design.

UNIT III: PHASE 1: DISCOVER 08 LECTURE HOURSBegin the design thinking process with the Discover phase, where you will identify the specific problem your design is intended to solve, as well as important usability aspects from those who will use your design. Discovery can be performed through a variety of different research methods which you will learn in this module.

UNIT IV: PHASE 2: DEFINE 08 LECTURE HOURSIn the Define phase, you come to understand the problem. We often refer to this as framing the problem. You can do this by using a variety of tools, including storytelling, storyboarding, customer journey maps, personas, scenarios, and more.

UNIT V: PHASE 3: DEVELOP 06 LECTURE HOURSTurn your attention to solving the problem. In this phase you brainstorm custom creative solutions to the problems previously identified and framed. To do this, you conceptualize in any way that helps, putting ideas on paper, on a computer, or anywhere whereby they can be considered and discussed.

UNIT VI: PHASE 4: DELIVER 06 LECTURE HOURSThis phase is all about testing and building concepts. Here you take all of the ideas that have been discussed to this point and bring them a little closer to reality by building a concept; something that makes it easier for a user to experience a design. This concept is referred to as a prototype.

UNIT VII: PHASE 5: ITERATE 08 LECTURE HOURSYou will test the prototype of your design solution, collecting and acting on feedback received. These actions may mean minor or major revisions to your design, and are repeated as often as necessary until a solution is reached. Tools such as focus groups and questionnaires are used to help you collect feedback that can help with your final design.

UNIT VIII: BEYOND DESIGN THINKING 06 LECTURE HOURSThe Design Thinking Model is a tool that helps guide you along a design thinking path. The model does this by providing a series of activities that that will help you effectively design a product, service or solution to a user’s need. The model presents the approach as a process, allowing us to look at each step – or phase – along the journey to the development of a final design.

Text Books1. All the references are available to download in the online course.

Reference Books1. Brown, Tim. “What We Can Learn from Barn Raisers.” Design Thinking: Thoughts by

Tim Brown. Design Thinking, 16 January 2015. Web. 9 July 2015.

2. Knapp, Jake. “The 8 Steps to Creating a Great Storyboard.” Co.Design. Fast Company & Inc., 21 Dec. 2013. Web. 9 July 2015.

3. van der Lelie, Corrie. “The Value of Storyboards in the Product Design Process.” Journal of Personal and Ubiquitous Computing 10.203 (2006): 159–162. Web. 9 July 2015. [PDF].

4. Millenson, Alisson. “Design Research 101: Prototyping Your Service with a Storyboard.” Peer Insight. Peer Insight, 31 May 2013. Web. 9 July 2015.

Modes of Evaluation: online discussion and assignmentsExamination Scheme: Continuous evaluation

All evaluation on the online course is done based on continuous basis for each of the 8 units/modules through out the semester. The assignment submission formats are in the form of qualitative discussion boards and online submissions of research data and developed product lifecycle and originally designed/redesigned prototype images.

Components Internal

Assessment

MSE ESE

Weightage (%) 0 0 100

Relationship between the Program Outcomes (POs), Program Specific Outcomes and Course Outcomes (COs) CO/PO

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

CO1 0 0 2 2 2 1 1 0 1 1 1 3 0 1CO2 0 0 2 2 2 2 1 0 1 1 1 3 0 0CO3 1 1 3 2 2 1 3 1 2 2 3 3 1 1CO4 0 0 3 3 3 3 3 1 2 2 2 3 0 1Average 0 0 3 2 2 1 2 1 1 1 2 3 0 1

1=Weakly mapped 2= Moderately mapped 3=Strongly mapped

HSFS 1001 Environmental Studies L T P CVersion 1.0 3 0 0 3Pre-requisites/Exposure a. Basics of Chemistry, Biology and Physics

b. General Observation, Discipline & AdaptabilityCo-requisites --

COURSE OBJECTIVES1. Understand environmental issues in multidisciplinary model. 2. Explain the natural environment and its relationships with human activities. 3. Analyze the impact of human activities on the environment. 4. Explain the structural and functional aspects of ecosystem. & identify the

types of ecosystems. 5. Explain the energy flow within the ecosystem using water, carbon, oxygen

and nitrogen cycles. 6. Identify the renewable and non-renewable resources. 7. Estimate the biological diversity of the environment & the threats to this

biological diversity. 8. Explain the various types of pollution. 9. Identify the causes of various types of pollution. 10.Analyse the harmful effects of various types of pollution. 11. Identify the treatment methods and controls for various types of pollution. 12. Evaluate and Explain on global environmental issues

COURSE OUTCOMES On completion of this course, the students will be able toCO1: Acquire the knowledge in those aspects of environmental science and ecology that are particularly valuable to bright young student, CO2: Fostering the development of analytical and technical skills in the environment, promoting a sense of responsibility and helping students deal effectively with ambiguity and disagreement about environment issues. CO3: Understand fundamental knowledge of various aspects of pollution and to motivate to adopt ecofriendly technologies to facilitate conservation and regeneration of natural resource. CO4: Create a pro-environmental attitude and behavioral pattern in the student that is based creating sustainable life styles.

CATALOG DESCRIPTIONEnvironmental Science, it is important for the students to have a knowledge about what is happening to the earth and its resources."The interdisciplinary course will be helpful in imparting knowledge to undergraduates from all educational backgrounds."It will not only give them a better understanding of environmental issues at the local, regional and global levels but also help them develop lateral thinking in this area.The subject gives a direct contact with nature and the knowledge of it: The subject environmental science gives students an ample scope for ‘application’. They will get some real-time knowledge and skill which required when they are actually dealing with environmental problems and the possible solutions. They can actually see the knowledge of physics and chemistry and for that matter even biology helps them to protect environment. This could give the student community a sense of ‘empowerment’.EVS encompasses many other science domains: In EVS we find a classic amalgamation of many other branches of science. This will expose students to a variety of theories and practical approaches thus enriching their knowledge.EVS encourages collaborative studies: When we talk about environmental issues we immediately realize that they are complex in nature. Such a thing will certainly chisel the analytical and problem solving skills of the students. Since the nature of environmental problems is both complex and critical, besides being huge, it demands team and collaborative work. This helps students to improve their interpersonal skills and they will emerge great leaders and team players in the future.Conscientizes students to the problems of the planet earth: The study of EVS could itself be conscientizing instrument in making students realize the peril of survival. Students might become aware of the danger that many may be unknowingly or ignorantly unleashing upon the planet we are living. In some ways it could be related to something called as “emancipator pedagogy’’ which makes students more insightful.

Course Content UNIT 1: MULTIDISCIPLINARY NATURE OF ENVIRONMENT STUDIES: 4

LECTURE HOURS

Multidisciplinary nature of Environmental Studies, scope, importance of environment & need of public awareness. Institutions in Environment, People in Environment.

UNIT 2: ECOSYSTEM: 6 LECTURE HOURSConcept of Ecosystem, Structure of ecosystem (Biotic and Abiotic) Biotic (Producer, Consumer and Decomposer), Abiotic (Physical factors & Chemical Factors) Functions of ecosystem Food Chain, Food Web, Trophic Level, Ecological Pyramid (Pyramid of energy, biomass, number) Energy flow in an Ecosystem, Biogeochemical cycle (cycling of nutrients)-, Carbon Cycle, Nitrogen cycle, Water Cycle, Oxygen Cycle, Carbon Cycle, Phosphorus cycle, Ecological Succession – Definition, Types of Succession, (Hydrosere and Xerosere) and Process of Succession.Major Ecosystem Types: Terrestrial Ecosystem: Taiga, Tundra, Deciduous, Grassland, Tropical Rain Forest, Desert, Aquatic Ecosystem: Fresh Water, (Lentic and Lotic Ecosystem) and Marine Ecosystem.

UNIT 3: NATURAL RESOURCES AND MANAGEMENT: 6 LECTURE HOURS Introduction of natural resources, Renewable and non-renewable resources, Renewable Energy: Wind, Power, Geothermal, Hydropower, Biomass, Biofuel, Non Renewable Energy: Petroleum, Natural Gas, Coal, Nuclear energy, Forest, Use of forest, Deforestation & Afforestation. Causes of Deforestation, Equitable use of resources for sustainable life style: Current and Future Global Challenges, Water (Surface water and ground water), Mineral resources.

UNIT 4: BIODIVERSITY & ITS CONSERVATION: 6 LECTURE HOURS Introduction of biodiversity, types of biodiversity (Genetic, Species and Ecosystem Biodiversity), Biogeographic Classification of India, Four Level Biogeographical Classification, (a) The Biogeographic Zone (b) The Biotic Province, (c) The Land Region (d) The Biome, India- A Mega- diversity nation, Ecoregion, Terrestrial Biome, Hot- Spots Biodiversity, Threats to Biodiversity, conservation of biodiversity (In - situ & Ex-situ), Case Study Project Tiger.

UNIT 5: ENVIRONMENTAL POLLUTION AND ITS CONTROL METHODS: 4 LECTURE HOURSEnvironmental Pollution, Types of Pollution, Causes, Effects and Control measures of Air pollution, Water pollution, Soil pollution, Noise pollution, Thermal pollution,

Radioactive pollution, Solid waste management- Causes, Effects and Control measures, Disaster Management (Flood, Earth Quake, Cyclone & Landslide).

UNIT 6: SOCIAL ISSUES AND ENVIRONMENT: 6 LECTURE HOURS Concept of sustainable development, (Concept, Principle and measures to Promote Sustainable Development), Climate changes, Global warming, Acid rain, ozone layer depletion, Carbon Foot Print, Ecological Foot Print, Environmental Impact Assessment, Environmental Protection Act, Air Prevention Act, The Water Prevention Act, The Wild Life Protection Act, Forest Conservation Act.

UNIT 7: HUMAN POPULATION & ENVIRONMENT: 4 LECTURE HOURS Population growth, Variation among Nations, Family Welfare Programme Global Population Growth, Population Explosion, Urbanization, HIV AIDS, Environment & Human Health, Value Education, Women & Child Welfare, Role of IT in Environment & Human Health, Case Studies.

Reference Books1. Text Book of Environmental Studies (Erach Bharucha), UGC, New Delhi2. Principles of Environmental Science & R.Pannir Selvam, SPGS, Chennai-600 088

Engineering.3. Encyclopedia of Ecology, Environment, Swaroop. R,Mishra, S.N. Mitlal, New Delhi

Jauri, V.P.4. Environmental Concerns, Saigo & Cunningham5. Air Pollution by M. N. Rao6. Environmental Studies: Kaur.H, Pragati Prakashan, Meerut


Components IA MSE ESEWeightage (%) 30 20 50

Relationship between the Program Outcomes (POs), Program Specific Outcomes (PSOs) and Course Outcomes (COs)

PO/CO

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

CO1 0 2 2 0 0 2 0 0 0 0 0 0 0 0

CO2 2 0 3 0 0 3 1 0 0 0 0 0 0 0

CO3 0 3 0 0 0 1 3 0 0 0 1 0 0 0

CO4 1 0 1 0 0 1 3 0 0 0 0 0 0 0

Average

1.5 2.5 2 0 01.75

2.33

0 0 0 1 0 0 0

1=Weakly mapped2= Moderately mapped3=Strongly mapped

MECH 1002 Engineering Mechanics L T P CVersion 3.0 3 0 0 3Pre-requisites/Exposure Basic Knowledge of physics.

Basic Knowledge of Mathematics & trigonometryCo-requisites --

COURSE OBJECTIVES1. Develop in the engineering student the ability to analyse any problem in a

simple and logical manner and to apply to its solution a few. 2. Analyze system of forces in statics.3. Understand the effect of friction on various engineering applications.4. Analyze the dynamics of a body under the action of various types of forces.5. Compute the kinematics of connected bodies.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Understand the basic concepts of statics and dynamics of rigid bodies. CO2. Apply the concepts of Engineering Mechanics in solving Engineering problems.CO3. Analyze forces, motion, work and energy problems and their relationship to engineering applications.

CATALOG DESCRIPTIONThe course covers the fundamental background in the statics and dynamics of rigid bodies, with a special emphasis on applications of laws of rigid body mechanics, as relevant to engineering sciences in general and automotive engineering in particular. The course begins with a description of basic laws of mechanics, resultant of system of forces and equilibrium of system. The aim is to develop in the engineering student the ability to analyze any problem in a simple and logical manner and to apply to its solution a few, well understood, basic principles. The application of concepts of mechanics further is elaborated in analysis of pinned joint structure and dynamics of bodies. Students will learn to understand the concepts of dealing problems with friction like belt, wedge and ladder friction. The understanding of centre of gravity and moment of inertia and its calculations are also explored in this course. Further, being a rigorous course on problem-solving, it will acquaint students with engineering problem-solving approaches and the effective use of commercial software packages to answer engineering questions.

Course Content

UNIT 1: RESULTANT AND EQUILIBRIUM OF COPLANAR FORCES 6 LECTURE HOURSBasic Concept and Principles of Mechanics, Types of force system, Composition and Resolution of Forces, Moments, Couple, Varignon’s Theorem, Equivalent Force System ,Type of body constraints, structural loads & supports , Free body diagrams, Condition of Equilibrium, Resultant and Equilibrium of Co-planner forces. Support reaction of simple & compound beams, Principle of virtual work

UNIT 2: CENTROID & MOMENT OF INERTIA 6 LECTURE HOURSIntroduction, Centroid and Moment of Inertia of composite plane figures

UNIT 3: PIN-JOINTED STRUCTURE 6 LECTURE HOURSIntroduction, perfect & imperfect frame, analysis of perfect frame by method of joint, method of section and graphical method

UNIT 4: FRICTION & LIFTING MACHINE 6 LECTURE HOURSIntroduction, Law of friction, simple contact friction on horizontal and inclined plane, Screw and Nut friction, Ladder, belt and wedge friction, Friction in journal collar bearings, Lifting Machines.

UNIT 5: KINEMATICS 6 LECTURE HOURSKinematics of Particle in Cartesian, polar and path co-ordinates, under uniform and non-uniform acceleration, Motion under gravity, Projectile Motion, Rotational motionKinematics of rigid bodies in two and three dimension, Instantaneous center of rotation

UNIT 6: KINETICS 6 LECTURE HOURSKinetics of Particle, Motion under constant force, Momentum and Energy principles, D-Alembert’s principle, Impulses and angular momentum, Motion under constant torque, Collision of Elastic bodies. Kinetics of general plane motion of body

Text Books:1. Tayal, A. K. “Engineering Mechanics Statics and Dynamics” 14th Edition, Umesh

Publications2. Bhavikatti, S. S. (2008) “Engineering Mechanics” New Age International (P) Limited,

Publishers.

Reference Books:1. Timoshenko, S., Young, D. H. and Rao, J. V. (2007) “Engineering Mechanics” Tata

McGraw Hill Publishing Company Limited, New Delhi2. Beer, F. P., Johnston, E. R., Mazurek, D. F., Cornwell, P. J., Eisenberg, E. R. and Sanghi,

S. (2011) “Vector Mechanics for Engineers: Statics and Dynamics” 9th Edition, Tata McGraw Hill Education Pvt. Ltd., New Delhi

3. Shames, I. H. and Rao, G. K. M. (2006) “Engineering Mechanics: Statics and Dynamics” 4th Edition, Pearson Education Inc.


Components Internal Assessment MSE ESEWeightage (%) 30 20 50


PO/CO

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

CO1 3 3 2 0 3 0 0 3 0 0 2 0 0 1CO2 3 3 2 0 3 0 0 3 0 0 2 0 0 1CO3 3 3 2 0 3 0 0 3 0 0 2 0 0 1Average 3 3 2 0 3 0 0 2 0 0 2 0 0 1

1=Weakly mapped2=Moderately mapped3=Strongly mapped

MEPD 1001 Workshop Technology L T P CVersion 3.0 2 0 0 2Pre-requisites/Exposure Basic Knowledge of physics, chemistry & MathematicsCo-requisites --

COURSE OBJECTIVES1. This course aims at imparting knowledge and skill components in the field of

basic workshop technology2. It deals with different hand and machine tools required for manufacturing

simple metal components and articles.3. To impart the knowledge regarding the various basic manufacturing

processes required in day to day life.4. To familiarize the students with the properties and selection of different

engineering material.

COURSE OUTCOMESOn completion of this course, the students will be able toCO1. Remember and identify basic tools and equipment used in engineering workshop.CO2. Understand the basic concepts of various manufacturing processes. CO3. Apply and relate the knowledge of manufacturing processes in fabrication of Engineering products.

CATALOG DESCRIPTION

Workshop technology is the backbone of the real industrial environment which helps to develop and enhance relevant technical hand skills required by the engineers working in the various engineering industries and workshops. This course intends to impart basic know-how of various hand tools and their use in different sections of manufacturing. Irrespective of branch, the use of workshop practices in day to day industrial as well domestic life helps to dissolve the problems. The workshop experiences would help to build the understanding of the complexity of the industrial job, along with time and skills requirements of the job. The students are advised to undergo each skill experience with remembrance, understanding and application with special emphasis on attitude of enquiry to know why and how for the various instructions and practices imparted to them in each shop.

Course Content

UNIT 1: ENGINEERING MATERIALS, ITS CLASSIFICATION 03 LECTURE HOURSFundamental learning about Metals/Non Metals, Ferrous and Non Ferrous, properties and Heat Treatment.

UNIT 2: HOT AND COLD WORKING 03 LECTURE HOURS Forging Shop, Introduction of Various Forging Operations; Drawing, Upsetting, Bending, Fullering, Swaging and Flattening.

UNIT 3: FOUNDRY SHOP 03 LECTURE HOURSIntroduction to Simple Pattern, Molding- Materials, Types, procedure of Mould preparation, use of Cores, Melting Furnaces, Tools and Equipment used in Foundry. NDT of castings.

UNIT 4: WELDING SHOP: 03 LECTURE HOURS Introduction to Different Welding Methods, Welding Equipment, Electrodes, Welding Joints, Awareness of Welding Defects. Gas/Electric Arc/Resistance & Special Types of wildings, Soldering and Brazing.

UNIT 5: FITTING SHOP: 03 LECTURE HOURSDescription of Fitting Tools and their uses, i.e. Hammers, Chisels, Files, Vices, Drills, Taps, Dies &Drilling machines.

UNIT 6: SHEET METAL SHOP: 03 LECTURE HOURSKnowledge of Tools and Equipment used in making of Sheet Metal Components and parts. Different joining Techniques.

UNIT 7: CARPENTRY SHOP: 03 LECTURE HOURSIntroduction to various types of timber, Ply-wood and Particle Boards, Defects in Timber, Seasoning of wood. Description and use of Carpenter’s Tools,

UNIT 8: MACHINE SHOP: 03 LECTURE HOURSIntroduction to various parts of Lathe, Lathe Tools and Lathe Operations. Demonstration of Thread Cutting, Drilling, Boring, Taper Turning and Knurling on the Lathe.

Text Books1. Hajra Choudhury, S. K. and Hajra Choudhury, A. K. (2015) “Elements of Workshop

Technology Vol 1& Vol 2” Media Promoters & Publishers Pvt Ltd.2. Khurmi, R. S. and Gupta, J. K. (2010) “Workshop Technology” S Chand Publisher

Reference Books 1. Raghuvanshi, B. S. (2015) “Workshop Technology Vol I &II” –Dhanpat Rai &

Publications Pvt Ltd2. Kalpakjian, S. (2014) “Manufacturing Engineering and Technology” Pearson Publisher




PO/CO PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

CO1 1 0 0 0 1 3 2 0 0 1 0 3 0 0CO2 3 0 2 0 3 1 2 0 0 2 0 3 0 0CO3 3 0 3 0 1 3 2 0 0 1 2 3 0 0Average 2.3

30 1.6

70 1.6

72.33

2 0 0 1.33

2 3 0 0


CHEM 1001 Chemistry L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure 12th level ChemistryCo-requisites --

COURSE OBJECTIVESObjectives of the course are:

1. To make students familiar with the fundamental concepts of chemistry. 2. To make the students understand the various basic chemical reactions,

related calculations and reasoning.3. To prepare the students for studying advanced subjects with required

knowledge of chemistry.

COURSE OUTCOMES On completion of this course, the students will be able to:

1. To know the basic concepts of chemistry w.r.t thermochemical reactions, reaction dynamics, organic reaction, electrolysis, electrochemical reactions, polymers and Nanomaterials

2. To explain preparation, properties, mechanism and case based reasoning in various chemical reactions and compounds/materials

3. To apply the concepts of chemistry in reaction dynamics, corrosion related problems and selecting suitable fuel for various domestic/industrial applications

4. To analyze the results of various analytical/chemical procedures

CATALOGUE DESCRIPTIONChemistry is present everywhere around us. It is existing in everything we see, feel or imagine. It is one of the very fundamental basics behind every structure, building, bridge, refinery and industry. In this course, focus will be on firming the basic knowledge of students about chemistry. Students will learn how to use the concepts correctly through prescribed syllabus. They will be taught various types of fuels. Different processes used to improve the quality of fuels in refineries will also be discussed. Combustion calculations related to oxygen or air required will help them to get an effective fuel:O2 ratio to result in proper and complete combustion. Kinetics will help them to understand the mechanism of reaction. This knowledge will make them able to control the factors to move the reaction in desired direction.

Corrosion is based on electrochemical cells. For any engineer, it is quite mandatory to have an understanding to select the suitable metal and also the methods to protect it from decaying. They will also be discussed about various types of polymers and nanomaterials so that they can correlate their properties to their various application areas. Course delivery will be made by classroom teaching, Blackboard, presentations, videos and tutorial classes.

Course Content UNIT I: FUELS & THERMOCHEMISTRY 8 LECTURE HOURS

Prerequisite: Enthalpy of formation, Enthalpy of neutralization and Enthalpy of combustion, Hess’s law of constant heat summation and its application, bond energyContents: Kirchoff’s equation, Fuels - Introduction, Classification and Characteristics, Important properties of a good fuels, Distillation of crude oil and petroleum composition, Important reactions for petroleum industries (isomerization, dimerization, aromatization, cracking), Calorific value, Determination of calorific value by Bomb calorimeter and Boys gas calorimeter, Combustion and its calculations, Flue gas calculations, Analysis of coal- proximate, Ultimate analysis, Octane number, cetane number

UNIT II: REACTION DYNAMICS 9 LECTURE HOURSPrerequisite: Rate of reaction and rate constant, factors affecting rate of a reaction, order and molecularity of a reaction, Rate expression for zero and first orderContents: Second (2A & A+B) and third (3A) order reaction, Methods of determining order of a reaction, Effect of temperature on reaction rate, Steady state approximation, Concept of activation energy and energy barrier, Collision theory, Kinetics of complex reactions- reversible, parallel, consecutive and chain reaction, Equilibrium and rate of reaction, Kinetics of polymerization reactions (step growth, chain growth, cationic, anionic and free radical polymerization)

UNIT III: ELECTROCHEMISTRY AND CORROSION 6 LECTURE HOURSPrerequisite: Galvanic cell, Single electrode potential, Nernst equation, ECS and its applicationsContents: Conductance and its types, Variation of conductance with dilution, Transport number (determination by Hittorf method & moving boundary method and

application in batteries), application of electrochemistry in corrosion (Introduction, dry theory, Wet theory, acid theory, types, Factors, prevention)

UNIT IV: ORGANIC CHEMISTRY 8 LECTURE HOURSPrerequisite: Inductive effect, Electromeric effect, Resonance and Hyperconjugation, Types of fission, Reactive intermediates Carbonium ion, Carbanions, Free radicalsContents: Types of organic reactions, Aliphatic nucleophilic substitution-SN1 and SN2, stereochemistry, Electrophilic substitution with energy profile- Halogenation, Nitration, sulphonation and Friedel craft reaction (comparison also), Addition reactions – electrophilic and nucleophilic, Elimination- E1 and E2, Elimination vs. substitution, mechanism of isomerization, Wolf-Kischner reduction and Clemmenson reduction, Fischer Trophs Synthesis.

UNIT V: POLYMERS 6 LECTURE HOURSPrerequisite: IntroductionContents: History, Classification, Physical properties, Types of polymerization, Copolymers, mechanism of polymerization (cationic, anionic and free radical), vulcanization, average molecular weight of polymers (end group analysis and osmotic pressure), biopolymers, conducting polymers, Polymeric electrolyte plastic hazards, plastic used in daily life applications

UNIT VI: NANOMATERIALS 3 LECTURE HOURSContents: Introduction, Methods of preparation, Effect on important properties, Application areas, BET Surface area, XRD

Text Books1. Bapna, Renu, Engineering Chemistry - New Delhi MacMillan 2010 – 431,

ISBN:0230330762.2. Text book of Engineering Chemistry, By: Chawla, Shashi,

BookPublisher: Delhi: Dhanpat Rai, 2014. ISBN 13: 123456755036.3. Engineering Chemistry, By: Krishnamoorty, P, Publisher: New Delhi: McGraw

Hill, 2012, Edition: 1.ISBN: 9780071328753.

Reference Books1. Encyclopedic dictionary of organic chemistry, By Milton, Jules K., Publisher: New

Delhi Pentagon Press 2004Description: 208p., ISBN: 818274167--X; 9788182741676.

http://ils.ddn.upes.ac.in:8001/cgi-bin/koha/opac-search.pl?q=Provider:Pentagon%20Press

http://ils.ddn.upes.ac.in:8001/cgi-bin/koha/opac-search.pl?q=an:%227249%22

http://ils.ddn.upes.ac.in:8001/cgi-bin/koha/opac-search.pl?q=Provider:McGraw%20Hill,

http://ils.ddn.upes.ac.in:8001/cgi-bin/koha/opac-search.pl?q=Provider:McGraw%20Hill,


http://ils.ddn.upes.ac.in:8001/cgi-bin/koha/opac-search.pl?q=Provider:Dhanpat%20Rai,

2. Crude oil chemistry, By: Simanzhenkov, Vasily, BookPublisher: New York: Marcel Dekker, 2003 Description: 409p.ISBN: 082474098.

3. Atkins' physical chemistry, By: Atkins, Peter, Paula, Julio De , BookPublisher: New Delhi Oxford University Press 2014, Edition: 10th. ISBN: 9780198728726; 0198728727.

4. Essentials of Physical Chemistry by Bahl & Tuli, Publisher: S.Chand & Co., ISBN 13: 978-8121929783.

5. Organic Chemistry for engineers, By: Mallick, Abhijit, Book Publisher: New Delhi: Viva Books, 2012, ISBN: 9788130920580.

Modes of Evaluation: Quiz/Assignment/ Common Class Tests/ Tutorial classes/ Written Examination Scheme:

Components MSE I IA (30) ESECCTs Tutorials/Assignment/ etc.

Weightage (%) 20 15 15 50


PO/COPO1 PO

2PO3 PO4 PO5 PO

6PO7 PO8 PO9 PO10 PO11 PO12 PSO1 PSO2

CO13 2 0 0 0 0 1 0 0 0 0 0 0 0

CO23 2 0 0 0 0 1 0 0 0 0 0 0 0

CO33 2 0 0 0 0 1 0 0 0 0 0 0 0

CO43 2 0 0 0 0 1 0 0 0 0 0 0 0

Average3 2 0 0 0 0 1 0 0 0 0 0 0 0


http://ils.ddn.upes.ac.in:8001/cgi-bin/koha/opac-search.pl?q=Provider:Viva%20Books,

http://ils.ddn.upes.ac.in:8001/cgi-bin/koha/opac-search.pl?q=Provider:Viva%20Books,


http://ils.ddn.upes.ac.in:8001/cgi-bin/koha/opac-search.pl?q=Provider:Oxford%20University%20Press



http://ils.ddn.upes.ac.in:8001/cgi-bin/koha/opac-search.pl?q=Provider:Marcel%20Dekker,

http://ils.ddn.upes.ac.in:8001/cgi-bin/koha/opac-search.pl?q=Provider:Marcel%20Dekker,


SEMESTER II

MATH 1004 MATHEMATICS II L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure Mathematics upto B.Tech 1st semester.

Co-requisites --

COURSE OBJECTIVES1. To help the students to solve the differential equations.2. To enable the students to understand the basic concepts of Laplace transforms3. To enable the students to understand the basic knowledge of vector calculus.4. To make the students to develop the basic knowledge of probability and statistics.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Solve the linear ordinary differential equations.CO2. Apply Laplace transform for the solution of linear ordinary differential equations and understand the basic properties of Fourier transform.CO3. Apply vector calculus techniques to evaluate line, surface and volume integrals.CO4. Interpret the engineering and scientific data using fundamental statistical techniques.

CATALOG DESCRIPTIONMathematics is necessary subject to a clear and complete understanding of virtually all phenomena. Its precision, depth, and generality support the development of critical thinking and problem-solving skills. This course provides a detailed knowledge of various methods to solve ordinary differential equations of constant as well as variable coefficients. This course also introduces the study of Laplace transform of various important functions. The students will also get insight into the solutions of boundary value problems using Laplace transform. In addition, this course will introduce the calculus of vector valued functions. The evaluation of line, surface and volume integrals has also been given in this course. The students will also get the basic knowledge of probability and statistics which is useful in engineering.

Course Content

UNIT I: ORDINARY DIFFERENTIAL EQUATIONS 9 LECTURE HOURSLinear Differential Equations with Constant Coefficients, Cauchy-Euler Differential Equations, Solution of Second Order Differential Equations (when a part of complementary function is known, by reduction to Normal Form, by changing the independent Variable and by Variation of Parameters)

UNIT II: INTEGRAL TRANSFORM 11 LECTURE HOURSLaplace Transform, Unit Step Function and Dirac-Delta Function, Periodic Functions, Differentiation and Integration of Laplace Transform, Inverse Laplace Transform, Convolution Theorem, and Solution of Linear Differential Equations, Fourier Transform.

UNIT III: VECTORS 9 LECTURE HOURSDifferentiation of vector valued functions and applications, Gradient, Divergence, Curl, and Integration of vector valued functions: Line, Surface and Volume Integrals, Applications of Green’s, Gauss divergence and Stokes Theorems.

UNIT IV: STATISTICS 13 LECTURE HOURSRandom Variable: Discrete and Continuous, Probability mass and Probability density Functions, Moments, Skewness and Kurtosis, Moment Generating Functions and their properties, Binomial, Poisson and Normal Distributions, Correlation: Karl-Pearson coefficient and Spearman Brown’s Rank correlation, Linear Regression and Chi Square Test.

Text Books1. J R. K. Jain and S. R. K. Iyengar, Advanced Engineering Mathematics, Narosa Publications.

ISBN: 9788184875607.2. E. Kreyszig, Advanced Engineering Mathematics, Wiley Publications. ISBN: 9788126531356.3. B. V. Ramana, Higher Engineering Mathematics, Tata McGraw Hill. ISBN: 9780071070089.

Reference Books

1. J. Stewart, Essential Calculus: Early Transcendentals, Cengage Learning India Pvt. Ltd. ISBN: 8131503453.

2. A. Jeffery, Advanced Engineering Mathematics, Academic Press, ISBN: 9780080522968.3. M. D. Greenberg, Advanced Engineering Mathematics, Pearson Education, India.

ISBN: 9788177585469.


Components Tutorial/Faculty Assessment

Class Tests MSE ESE

Weightage (%) 15 15 20 50


CO/PO

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

CO1 3 2 0 0 2 0 0 0 0 0 0 0 0 0CO2 3 2 0 0 2 0 0 0 0 0 0 0 0 0CO3 3 2 0 0 2 0 0 0 0 0 0 0 0 0CO4 3 2 0 0 2 0 0 0 0 0 0 0 0 0Average 3 2 0 0 2 0 0 0 0 0 0 0 0 01. WEAK 2. MODERATE 3. STRONG

PHYS-1004 Physics II L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure 12th level PhysicsCo-requisites 12th level Mathematics

COURSE OBJECTIVES1. To develop an understanding in the space and time relations and to apply Lorentz transformations to comprehend the outcome of Special Theory of Relativity.2. To Systematically introduce the basic principles of Quantum mechanics and apply to various systems.3. To develop working knowledge of elementary statistical mechanics and its application in exploring various Classical and Quantum phenomenon.4. To demonstrate the fundamentals of Semiconductor Physics that will subsequently enable students to understand the characteristics of Semiconductor devices.5. Introduce basic principles of dielectric and magnetic properties of solids and their applications.

COURSE OUTCOMES On completion of this course, the students will be able toCO1: To understand the need of various mechanics e.g. relativistic, quantum and statistical in addition to physics of semiconducting, dielectric and magnetic properties of materials. CO2: To calculate various physical parameters related to physics of atomic scale and high speed particles using relevant mechanics and to solve the problems related to semiconducting, dielectric and magnetic materials CO3: To apply the concepts of relativistic, quantum and statistical mechanics in physics problems and in various physical situations. CO4: To analyze the behavior of various parameters of various material properties in view of applicable mechanics.

CATALOG DESCRIPTIONAlmost all disciplines of engineering and technology have origins in basic principles of Physics. Furthermore special theory of relativity instigates an out-of-box thinking habit among the students. Quantum Mechanics describes physical phenomena in which the wave and particle aspects of matter and radiation are reconciled in a unified manner. The knowledge of the Quantum Mechanics can be applied to the

study of optical and electronic sensor as well as to study the behavior at microscopic and nano level. The behavior of system of particles at different physical variables (such as temperature, pressure, volume, velocity etc.) can be understood with the help of statistical mechanics, therefore course provides the information about different types of materials available for various applications. The role of semiconductors in the development of various electronic devices, sensors, computer hardwares, etc., which has made our lives easier, has been commendable. The course lays a sound foundation to develop an understanding about functioning mechanism of basic components such as diodes, LED, transistors as well as Photovoltaic cells. Photovoltaic cells are nowadays employed to generate clean energy from solar power. The course also provides an emphasis on the materials (such as dielectric, capacitors and magnetic materials) required for storing charges as well as memory devices.

Course Content UNIT I: 16

LECTURE HOURSModern physics and introductory quantum mechanics- Inertial & Non-inertial frames, Postulates, Lorentz transformations, Length contraction, Time dilation, velocities addition, variation of mass with velocity, Mass-energy equivalence and Energy momentum relation.Introduction, photoelectric effect, Compton Effect, Pair production & Annihilation, De-Broglie waves, Waves of probability, phase and group velocities, Thought Experiment; Electron microscope, particle diffraction, Uncertainty principle and its applications, Two-slit interference experiment, Wave function and its interpretation, Normalization, Schrodinger time independent & dependent wave equations, Linearity and superposition, expectation values, operators, Eigen values &Eigen functions, Particle in a 1-D box, generalization to 3-D box.

UNIT II: 10 LECTURE HOURSStatistical and thermal physics- Introduction to Statistical Physics, Statistical Distribution, Maxwell Boltzmann Statistics, Probability function, density of state, Applications of MB Statistics: Average molecular energy, Distribution of molecular speeds vrms, vav, vmp, Quantum Statistics, B-E Statistics, Probability function, density of state, Rayleigh Jeans Formula, Planck Radiation Law & Specific Heat of

solids, Fermi Dirac Statistics, Probability function, density of state, Fermi energy, electron-energy distribution.

UNIT III: 7 LECTURE HOURSSemiconductor physics- Introduction to semiconductors, momentum energy diagram for band gap explanation P and N Type semiconductors, direct and indirect band gap materials, Hall effect, P-N junction diode, forward and reverse biasing of P-N junction diode, Shockley equation, Avalanche breakdown, Zener breakdown, Zener diode, Photodiode, Photovoltaic effect, LED construction and materials.

UNIT IV: 9 LECTURE HOURSDielectric and magnetic materials- Electric susceptibility, dielectric constant, electronic, ionic, orientational and space charge polarization, frequency and temperature dependence polarization, internal fields, Claussius and Mosotti relation (derivation), dielectric loss, dielectric breakdown, use of dielectric materials in capacitor and transformer, Ferroelectricity and applications. Origin of magnetic moments, Bohr magnetron, comparison of dia, para and ferro magnetism, domain theory, hysteresis, soft and hard magnetic magnetic materials, antiferromagnetic materials, ferrites and its applications.

Text Books1. Mehta N., (2009) Text Book of Engineering Physics Part-1. PHI Learning Pvt. Ltd.

ISBN: 9788120333611.2. Beiser A., Mahajn S., Chaudhury S. R., (2009) Concepts of Modern Physics, 6th ed. McGraw Hill

Education Pvt. Ltd. ISBN: 9780070151550.3. Vasudeva A.S., (2010) Modern Engineering Physics (Revised Edition), S. Chand & Company

Ltd. ISBN: 9788121917575.4. Jain A. K, Malik H. K., (2016) Engineering Physics, Tata McGraw-Hill Education Pvt.

Ltd. ISBN: 9780070671539.

Reference Books

1 Griffith D.J. (2012) Introduction to Electromagnetics, PHI Learning, 4th edition, ISBN: 9780138053260

2. Pillai S.O., (2009) Solid State Physics, 6th ed. New Age International Pvt. Ltd. ISBN: 9781906574109.


Components CCT Tutorial/Assignments MSE ESE

Weightage (%) 15 15 20 50


PO/COPO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO 11 PO12 PSO1 PSO2

CO13 0 0 0 0 0 0 0 0 0 0 0 0 0

CO23 2 0 0 0 0 0 0 0 0 0 0 0 0

CO33 2 0 0 0 0 0 0 0 0 0 0 0 0

CO43 2 0 0 0 0 0 0 0 0 0 0 0 0

Average

3 2 0 0 0 0 0 0 0 0 0 0 0 0


COMM1001 English Communication L T P CVersion 1.0 2

(Online)0 2 4

Pre-requisites/Exposure K12 knowledge of the English LanguageCo-requisites Knowledge of Word processing using MS Word, basic IT skills

COURSE OBJECTIVESThe Objectives of this course are:

1. To develop a holistic view of communicating in English Language both written and verbal.

2. To help the second language learners develop the ability to understand spoken language through machine and task based activities.

3. To enable students to communicate with clarity and precision through proper understanding of technical and academic writing techniques.

4. To study and understand applicative grammar and its various structures for correct usage of English Language.

COURSE OUTCOMES On completion of this course, the students will be able to:CO1 Comprehend and summarize various structural principles of English Grammar, prerequisite to English Communication.CO2. Evaluate and apply the acquired learning of remedial Grammar for self-expression and diverse communication purposes. CO3. Identify and analyze the nuances of English Language prerequisite to Scientific and Technical Writing. CO4. Apply appropriate Language skills for developing scientific and technical content using academic and experimental approaches.CO5. Comprehend and analyze receptive & productive skills based on various task-based and machine-based activities.CO6- Apply and Formulate scenario based forms of Content for English Language learning and presentation.

CATALOG DESCRIPTIONThis course focuses on the development of students’ English language, Communication and Critical thinking skills through the understanding of Language viz. Listening, Speaking, Reading and Writing. The course enables the students to

appreciate the nuances of Academic and Technical writing through an understanding of principles and structures of Applicative Grammar. Students will be assessed on their demonstration based on Language learning skills. The course is offered on blended mode.

Course Content UNIT 1: GRAMMAR+ 12 LECTURE HOURS

(ONLINE) An overview on the basics of Grammar : Different aspects of grammar and

usage of correct English Articles and Prepositions: Identification and correct usage in writing Tenses – 1, 2 & 3: Types and correct use of different tenses Simple, Compound and Complex Sentences: Usage and types of sentences Active and Passive Voice: Usage and conversion in different contexts Conditional Sentences : Types and usage of sentences Question Tags: Identify and use correct question tags Phrasal Verbs: Identify and use phrasal verbs correctly Idioms: Usage to enrich expression Blog and online content development

UNIT 2: TECHNICAL COMMUNICATION 12 LECTURE HOURS (ONLINE)

Scientific English –Pre-requisite to technical writing: Nature, Use of Language, Organization

Scientific English – Nuances: Sentence Structure and Paragraph Development Generalization – Nature, Induction and Deduction method Classification – Nature, Writing classifications and generalizations Definition – Nature, Types, Writing definitions and generalizations Comparison & Contrast – Ways of expressing comparison and contrast Instructions – Language and types, Instructions and reporting Descriptions – Description of substances, objects and processes Narratives – Nature, Writing of narratives, Organization Explanations – Nature, Writing explanations Hypotheses – Nature, Hypothesis and predictions, Writing hypothesis Technical Poster Making

UNIT 3: LANGUAGE WORKSHOP 24 LECTURE HOURS (F2F)

Introduction to Language Workshop Sessions and its usage in improving language proficiency & Self-Expression techniques

Listening Skills: Basic Ear Training. Listening to Received Pronunciation, Attention to Accuracy: Situational Conversations/Role Play/Development of Argumentative Skills

Speaking Skills: Individual Introduction to IPA symbols, basic training for correct Pronunciation pattern, Official/Public Speaking with emphasis on correct speech patterns, common errors in reading and speaking with emphasis on Para linguistics, developing impromptu Skills in speaking.

Reading Skills: Skimming and Scanning: Comprehension Skills based on practice Reading Comprehension.

Writing Skills: Writing for Purpose (Objective/Subjective) with special emphasis on Grammar and Vocabulary Building Exercises

Text Books1. Mishra. B, Sharma. S (2011) Communication Skills for Engineers and Scientists. PHI

Learning Pvt. Ltd. ISBN: 8120337190.2. Academic Writing: A course in English for Science and Technology – Rizvi, M.H. -

TMHMishra. B, Sharma. S (2011)3. Reddy, S.D.(2009). Technical English. Macmilan Publishers: New Delhi. ISBN:

0230639119.4. Flatley, M.E. (2004). Basic Business Communication, Skills for empowering the Internet

Generation.Tata McGraw Hills: New Delhi. ISBN: 9780070486942.5. Wren & Martin, M.E. (2006). High School English Grammar & Composition. Tata S.

Chand & Company LTD: New Delhi. ISBN: 9788121924894.

Reference Books1. Pal, Rajendra and Korlahalli, J.S. (2011) Essentials of Business Communication. Sultan

Chand & Sons. ISBN: 9788180547294.2. Kaul, Asha. (2014) Effective Business Communication.PHI Learning Pvt. Ltd. ISBN:

9788120338487.3. Murphy, R. (2007) Essential English Grammar, CUP. ISBN: 8175960299.4. C. Muralikrishna and S. Mishra (2011) Communication Skills for Engineers, Pearson

education. ISBN: 9788131733844.5. Essential English Grammar by Raymond Murphy, CUP, 20116. Intermediate English Grammar by Raymond Murphy, CUP, 20117. Practical English Usage by Michael Swan, OUP, 20138. Jones, D. (1909), "The Pronunciation of English", Cambridge: CUP; rpt in facsimile in

Jones (2002).

9. Jones, D.(1918), "An Outline of English Phonetics", Leipzig: Teubner; rpt in Jones (2002).

10. Jones, D. (1909) “The Dictionary of English Phonetics” Cambridge: CUP (2002).11. Bansal, R.K. The Intelligibility of Indian English, Monograph, 4 CIEFL, Hyderabad,

Second abridged edition, 1976.12. Jones, Daniel, English Pronouncing Dictionary, revised by A.C. Gimson, 14th Edition,

The English Language Book Society and JM Dent Sons Ltd. London 1977.13. Senthi. J and P.V. Dhamija, A Course in Phonetics and Spoken English Prentice hall of

India Private Ltd. New Delhi, 1989.14. Taylor, Ken, Telephoning and Teleconferencing Skills. Orient Black Swan, 2008.15. Dignen, Bob. Presentation Skills in English. Orient Black Swan, 2007.

Modes of Evaluation: Online Discussion/Quiz/Assignment/Blog/Listening, speaking, reading, writing examination.Examination Scheme:

Components Mid-term (Grammar+)

IA (Technical Communication)

End-term (Language Workshop)

Weightage (%) 20(3 Online Discussions, 4 Online Quiz)

30(2 Online Discussion, 1 Online Assignment, 3 Online Quiz)

50(4 Continuous Evaluation)


PO/CO PO1 PO2PO3

PO4 PO5 PO6PO7

PO8 PO9 PO10PO 11

PO12 PSO1PSO2

CO1 0 0 0 0 0 0 0 0 0 3 0 0 0 0

CO2 0 0 0 0 0 0 0 0 0 3 0 2 0 0

CO3 0 0 0 0 0 0 0 0 0 3 0 0 0 0

CO4 0 0 0 0 0 0 0 0 0 3 0 0 0 0

CO5 0 0 0 0 0 0 0 0 1 3 0 0 0 0

CO6 0 0 0 0 0 0 0 0 1 3 0 0 0 0

Average

0 0 0 0 0 0 0 01 3

0 2 0 0

1=weakly mapped2= moderately mapped3=strongly mapped

MECH1001 Engineering Graphics L T P CVersion 3.0 1 0 2 2Pre-requisites/Exposure The knowledge of simple geometrical theorem and

procedures is essential.Co-requisites --

COURSE OBJECTIVES1. Increase ability to communicate with people.2. Enhance knowledge, imagination and drawing skill.3. Learn basics of design software Solid works skills.4. Draw the accurate and precise line drawing.5. Prepare the student for future Engineering positions.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Remember the conventions of engineering graphics such as types of lines, dimensioning, method of projection etc.CO2. Demonstrate understanding of fundamental concepts of engineering graphics.CO3. Apply knowledge of orthographic and isometric projections to solve problems related to points, lines, planes and solids.CO4. Analyze the basic Engineering drawings

CATALOG DESCRIPTIONEngineering graphics builds the foundation of analytical capabilities for solving a great variety of engineering problems involving diagrams. It also has numerous real time application in almost all branches of engineering. This subject helps the student to enhance their knowledge, imagination and drawing skill. The purpose of the study of the engineering graphics is to develop the ability to visualize an object with physical and dimensional configurations. With its extensive coverage, the step-by-step approach and handy drawing tips. The subject support for students to draw the accurate and precise line drawing.

Course Content UNIT 1: INTRODUCTION OF ENGINEERING DRAWING, LINES, LETTERING AND

DIMENSIONING 1 LECTURE HOURSIntroduction, Drawing instruments, Drawing sheet, pencils, Sheet layout, Title Block, Configurations of lines, drafting of lines, Types of lines and their applications, Order

of priority of coinciding lines, Lettering, Dimensioning, terminology and method of execution, placing and general rule of dimensioning.

UNIT 2: ORTHOGRAPHIC PROJECTIONS: 1 LECTURE HOURSProjection, Pictorial view and Multi view, Orthographic Projection, Multi View Projection, Terminologies, First-Angle Projection, Third angle Projection, Second angle and Fourth angle Projection, Symbols of Orthographic Projection

UNIT 3: PROJECTION OF POINT: 1 LECTURE HOURSIntroduction, Conventional Representation, A point situated in first quadrant (above HP and in front of VP), A point situated in second quadrant (above HP and behind VP), Point in the third quadrant (below HP and behind VP), Point in the Fourth quadrant (below HP and in front of VP). Problems

UNIT 4: PROJECTION OF LINES: 2 LECTURE HOURSOrientations of straight lines, lines parallel to one or both the planes, line contained by one or both the planes, Line perpendicular to either of the RPs, line inclined to one RP and parallel to other, line inclined to both the RPs, Traces of a line, Methods of determining traces of line.

UNIT 5: PROJECTION OF PLANES: 2 LECTURE HOURSIntroduction, Position of Planes, Terms used in projection of planes, Planes parallel to an RP, Plane inclined to one RP and perpendicular to the other RP, plane perpendicular to both the RPs, Plane inclined to both the RPs, Suspended planes, Traces of planes,

UNIT 6: PROJECTION OF SOLIDS: 2 LECTURE HOURSIntroduction, Basic solids, Frustums and Truncated Solids, position of the solids, solids with Axis perpendicular to an RP, Solid with Axis inclined to one RP and parallel to the other, solid with axis inclined to both the RPs, solid with axis parallel to both the RPs, Rules for deciding the Hidden Lines

UNIT 7: SECTION OF SOLIDS: 2 LECTURE HOURSSection planes, Sections, True shape of a section, Section of prisms: section plane parallel to VP, Section plane parallel to the HP, Section plane perpendicular to HP and inclined to the VP, Section plane perpendicular to the VP and inclined to the HP. Sections of Pyramids, Sections of cylinders, sections of cones etc.

UNIT 8: ISOMETRIC PROJECTION: 1 LECTURE HOURIntroduction, Principle of Isometric Projection, Terminology, Isometric Scale, Isometric Projections and Isometric Views.

Text Books1. Bhatt, N. D. (2014) “Engineering Drawing”, Charol Publication2. Gill, P. S. (2009) “Engineering Drawing”, Kataria Publication3. Dhawan, R. K. (2011) “Engineering Drawing”, S Chand

Reference Books1. Morling, K. “Geometric and Engineering Drawing”, Third Edition, Elsevier 32

Jamestown Road London NW1 7BY 30 Corporate Drive, Suite 400, Burlington, MA 01803, USA

Modes of Evaluation: Quiz/Assignment/ presentation/ extempore/ Written Examination

Examination Scheme:



PO/CO

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11 PO12

PSO1 PSO2

CO1

3 3 3 2 3 0 0 0 0 2 0 0 0 0

CO2

3 3 3 2 3 0 0 0 0 2 0 0 0 0

CO3

3 3 3 2 3 0 0 0 0 2 0 0 0 0

CO4

3 3 3 2 3 0 0 0 0 2 0 0 0 0

Average

3 3 3 2 3 0 0 0 0 2 0 0 0 0


ECEG 1001 Basic Electrical & Electronics L T P CVersion 6.0 3 0 0 3Pre-requisites/Exposure a. Basic Knowledge of fundamentals of electrical

components and Engineering Mathematicsb. Basic knowledge of electronics and digital

components.Co-requisites --

COURSE OBJECTIVES On completion of this course, the students will be able to

1. The capability to design and construct circuits, take measurements of circuit behaviour and performance, compare with predicted circuit models and explain discrepancies.

2. To impart the basic knowledge about the Electric and Magnetic circuits.3. To inculcate the understanding about the AC fundamentals and understand

various Electrical Machines.4. Employ electronic components and devices to solve the Engineering

problems.5. Analyse and make simple Circuits and Systems of Electronics Engineering, To

Interpret the logics used in the Digital Circuits and Systems.6. Design the electronics system with discrete component and to understand the

specifications of industrial equipment.

COURSE OUTCOMESCO1: The capability to design and construct circuits, take measurements of circuit behaviour and performance, compare with predicted circuit models and explain discrepancies.CO2: Impart the basic knowledge about the Electric and Magnetic circuits.CO3: Inculcate the understanding about the AC fundamentals and understand various Electrical Machines.CO4: Employ electronic components and devices to solve the Engineering problems.CO5: Analyse and make simple Circuits and Systems of Electronics Engineering, Interpret the logics used in the Digital Circuits and Systems.CO6: Design the electronics system with discrete component and to understand the specifications of industrial equipment.

CATALOG DESCRIPTIONElectrical & Electronics is the integral part of life. The basic circuits used in day to day life are studied in this course. In this course, the main focus will be on the designing of basic electrical and electronics circuits like AC to DC converter by using diode, half adder, full adder etc. in Electronics and three phase system circuits in electrical. Students will learn how to use diode, transistor, Integrated circuit, AC machine and DC Machine in real time and develop circuits buy using them. Classroom activities will be designed to encourage students to play an active role in the construction of their own knowledge and in the design of their own learning strategies. We will combine traditional lectures with other active teaching methodologies, such as practical sessions, group discussions, and cooperative group solving problems. Class participation is a fundamental aspect of this course. Students will be encouraged to actively take part in all practical sessions to apply the devices and design the basic circuits.

Course Content UNIT 1: CIRCUIT COMPONENTS AND CIRCUIT ANALYSIS 10

LECTURE HOURSINTRODUCTION: Resistance, inductance and capacitance, open circuit and short circuit, electrical power and energyDC CIRCUIT: Ohm’s law. Kirchhoff’s law, series and parallel network, network theorems: Thevenin’s, Norton, Maximum Power and SuperpositionAC CIRCUITS: Single Phase and Three Phase Circuits, Star Delta connections, Concept of power factor, series and parallel network, resonance.

UNIT 2: CONCEPT OF ELETROMAGNETIC INDUCTION 5 LECTURE HOURSFlux, flux density, reluctance, mmf, magnetic field strength Fleming left hand rule, Fleming’s right hand rule, faradays law, statically and dynamically induced emf. Eddy current and Hysteresis loss.

UNIT 3: POWER SYSTEM OVERVIEW 7 LECTURE HOURSElectrical Machines construction, operation, characteristic and application Transformer, Induction Motor, DC Machines, Electrical Power Generation, Transmission and Distribution. Basic Layout of Power System and various voltage levels at different sections of Power System.

UNIT 4: DIODES AND DIODE CIRCUIT 7 LECTURE HOURSIntrinsic and Extrinsic Semiconductors; Formation and Fundamental Characteristics of diode: Formation of P-N junction, I-V characteristics, Zener and Avalanche breakdown; half-wave and full-wave rectifier circuits; dc-power supply design and diode applications.

UNIT 5: BIPOLAR JUNCTION TRANSISTORS 6 LECTURE HOURSTransistor construction and operation, Common-Base (CB) configuration, Transistor amplifying action, Common Emitter (CE) configuration, Amplification factors for CB and CE configurations, Common Collector configuration, Limits of operation, DC-Biasing: Fixed bias, Emitter bias, Voltage divider bias, Applications:

UNIT VI: DIGITAL LOGICS AND CIRCUITS 5 LECTURE HOURSNumber system and codes, Boolean algebra and minimization techniques: Boolean logic operations, Basic laws of Boolean algebra, Demorgan’s Theorems; Logic gates: AND, OR, NAND, NOR. Adders and sub-tractor.

Text Books1. Electrical & Electronics Engineering by K R Niazi,Genius

Publication.ISBN:97881888701372. Basic Electrical and Electronics Engineering, by J B Gupta S K Kataria and Sons.3rd Ed.3. Electronics Devices and Circuits By Boylestad & Nashelsky 10th ED : PEARSON: ISBN

978-8131727003Reference Books

1. Basic Electrical Engineering by Chakrabarti, Tata McGraw Hill. ISBN: 97812590833652. Basic Electrical Engineering by U.A.Bakshi, V.U.Bakshi, ISBN: 97881843169403. A Text Book of Electrical Machines by Rajput, L P Publications. ISBN: 97881318044694. Basic Electronics By Santiram Kal,( 2013): PHI5. Digital Circuits & Logic Design By Salivahanan: Vikas Publishing House. ISBN 978-

9325960411




PO/CO PO1 PO2PO3

PO4 PO5 PO6 PO7 PO8 PO9PO1

0PO 11

PO12

PSO1

PSO2

CO1 3 3 2 1 1 0 0 0 0 0 0 1 0 0

CO2 3 3 2 1 1 0 0 0 0 0 0 1 0 0

CO3 3 3 2 1 1 0 0 0 0 0 0 1 0 0

CO4 3 3 2 1 1 0 0 0 0 0 0 1 0 0

CO5 3 3 2 1 1 0 0 0 0 0 0 1 0 0

CO6 3 3 2 1 1 0 0 0 0 0 0 1 0 0

Average

3 3 2 1 1 0 0 0 0 0 0 10 0

1=weakly mapped 2= moderately mapped 3=strongly mapped

CSEG 1001 Computer Programming L T P CVersion 1.0 3 0 0 3Pre-requisites/Exposure Fundamentals of ComputerCo-requisites Mathematics

COURSE OBJECTIVES1. To help the students to understand and identify the functional units of

Computer System. 2. To enable students to understand the concepts of procedure oriented

programming using C Language.3. To empower students with the expertise of experimentation using C

programming skills.4. To expose students with the ability to design programs involving decision

structure, loops and functions.5. To equip students with necessary engineering skills such as solving

engineering problems through implementing concepts of arrays, pointers, structures and union in C programming Language.

COURSE OUTCOMES CO1. Comprehend the concepts of flowcharts and algorithms along with decision constructs through programming techniques in C.CO2. Identify various concepts of Programming like arrays, strings, and matrix operations.CO3. Apply concepts of functions and pointers to resolve mathematical problems using C.CO4. Demonstrate the concept of Structures and Unions using C programming.

CATALOG DESCRIPTIONComputer Programming is rapidly gaining the importance in the field of education and engineering. The course will introduce to the students about computer programming language and the fundamentals of computer programming. This subject is designed specifically for students with no prior programming experience and taking this course does not require a background in CS. This course will touch upon a variety of fundamental topics within the field of Computer Science and will use ‘C’ programming language to demonstrate varied principles. We will begin with an overview of the course topics as well as brief history of computers. We will cover

basic programming terminology and concepts related to C language. By the end of the course, students should have a strong understanding of the fundamentals of C programming language. This course will help the students to build up a strong background in programming skills and a successful career devoted to implementing the principles they will learn. Students will learn effectively through prescribed syllabus as well as through blackboard and discussions. Classroom activities designed to encourage students to play an active role in the construction of their own knowledge. The students will be able to design their own learning strategies through online learning management system – blackboard. We will combine traditional lectures with other active teaching methodologies, such as group discussions, cooperative group solving problems. Class participation is a fundamental aspect of this course. Students will be encouraged to take part in all group activities to meet the course outcome. Students expected to interact with media resources, such as, web sites, videos, DVDs, and newspapers, etc.

Course Content UNIT 1: INTRODUCTION 7

LECTURE HOURSGeneration and classification of computers, Basic computer organization, Number system – binary, decimal conversion problem, Need for logical analysis and thinking, Algorithm, pseudocode, flowchart.

UNIT 2: C PROGRAMMING BASICS 8 LECTURE HOURSProblem formulation, Problem Solving, Introduction to C Programming fundamentals, Structure of a C Program, Compilation and Linking processes, Constants, Variables, Data types – Expressions using operators in ‘C’, Managing input and output operations, Decision making and branching, Looping statements, solving simple scientific and statistical problems.

UNIT 3: ARRAYS AND STRINGS 7 LECTURE HOURSArrays – initialization, Declaration one dimension and two dimensional arrays, string and string operations, string arrays, simple programs – sorting, searching, matrix operations.

UNIT 4: FUNCTIONS AND POINTERS 6 LECTURE HOURS

Functions – definition of function, Declaration of function, Pass by value, Pass by reference, Recursion, Pointers – Definition, Initialization, Pointers arithmetic, Pointers and arrays, Example, problems.

UNIT 5: STRUCTURE AND UNION 8 LECTURE HOURSIntroduction - need for structure data type, Structure definition, Structure declaration, Structure within a structure, Union, programs using structure and unions, Storage classes, preprocessor directives.

Text Books1. Reema Thareja, Computer Fundamentals & Programming in C, Oxford Press.2. Yashwant Kanetkar, Let Us C, BPB Publications.

References 1. Herb Schildt, The Complete reference C. 2. Byron Gottfried, Programming with C, Schaum’s Series.3. K.R. Venugopal and S. R. Prasad, Mastering ‘C’4. http://learn.upes.ac.in Blackboard – LMS

Modes of Evaluation: Quiz/Assignment/Discussion/ Online ExaminationExamination Scheme:



PO/CO

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11 PO12

PSO1 PSO2

CO1

3 2 1 0 1 0 0 0 0 0 1 0 0 0

CO2

3 2 1 0 1 0 0 0 0 0 1 0 0 0

CO3

3 2 1 0 1 0 0 0 0 0 1 0 0 0

CO4

3 2 1 0 1 0 0 0 0 0 1 0 0 0

Average

3 2 1 0 1 0 0 0 0 0 1 0 0 0

1=weakly mapped2= moderately mapped

http://learn.upes.ac.in/

3=strongly mapped

SEMESTER III

MATH 2001 Mathematics-III L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure Mathematics upto B.Tech 1st yearCo-requisites --

COURSE OBJECTIVES1. To help the students develop the concept of difference equations and their

solution.2. To enable the students understand the series solution of second order

differential equation.3. To make the students able to investigate the behaviour of complex variable

functions.4. To enable the students to understand the use of analytic functions in

evaluating complex and real integrals.5. To make the students able to solve PDEs and its applications.

COURSE OUTCOMESOn completion of this course, the students will be able toCO1. Find the solution of linear difference equations.CO2. Solve linear second order differential equations using series solution method and comprehend the Legendre’s polynomials, Bessel functions, its related properties CO3. Explain the concepts of analyticity, integration of a complex function and conformal mapping.CO4. Find the series representation of a complex function CO5. Evaluate real integrals using calculus of residues.CO6. Solve homogeneous partial differential equations with constant coefficients and its applications in one dimensional heat and wave equations.

CATALOG DESCRIPTIONThis course covers the difference equations, ordinary differential equations, partial differential equations and complex analysis. The difference equations will be solved using operator method, generating function technique and matrix method. The solution of second order linear differential equations will be obtained using series solution method and the properties of special functions like Legendre’s polynomials and Bessel’s functions will be investigated. In addition, this course will introduce the calculus of complex functions of a complex variable. It turns out that complex differentiability is a very strong condition and differentiable functions behave very

well. The central result of this spectacularly beautiful part of mathematics is Cauchy's Theorem guaranteeing that certain integrals along closed paths are zero. This striking result leads to useful techniques for evaluating real integrals based on the 'calculus of residues'. Charpit method ensures the solution of first order nonlinear partial differential equations and separation of variables method useful to solve the one dimensional wave and heat equations.

Course Content UNIT I: DIFFERENCE EQUATIONS AND ORDINARY DIFFERENTIAL EQUATIONS

12 LECTURE HOURSIntroduction, formulation, homogeneous and non-homogeneous difference equations, Solution by Operator method, Solution by Generating function technique, Solution by Matrix method, Introduction of series solution, Power series method, Frobenius method and its cases, Series solution of Legendre’s and Bessel’s Des, Legendre polynomials, Bessel functions and its Properties.

UNIT II: COMPLEX VARIABLES-I 9 LECTURE HOURSIntroduction to functions of a complex variable, Notion of limit, continuity and differentiability, Analytic function and CR equations, Necessary & sufficient conditions for analyticity, Harmonic function, harmonic conjugate and orthogonal families, construction of an analytic, function using Milne Thomson method, Line integral where curve defined in parametric, form, explicit function, Path independence for a contour integral, Cauchy’s theorem, Cauchy-Goursat theorem for simply and multiply connected domain, Cauchy’s integral formula for the derivatives of an analytic function.

UNIT III: COMPLEX VARIABLES-II 12 LECTURE HOURSTaylor’s and Laurent’s series, Zeros and poles of a function, the residue at a singularity, Cauchy Residue Theorem, Contour integration and its applications to improper integrals, evaluation of a real integrals, improper integrals involving sines and cosines, definite integrals involving sines and cosines, Image under translation, rotation, magnification/contraction, inversion, Definition of Conformal mapping and Bilinear, transformation , Cross ratio.

UNIT IV: PARTIAL DIFFERENTIAL EQUATIONS 9 LECTURE HOURS

Formation of PDE by elimination of arbitrary constants and arbitrary functions and classification of PDEs, Lagrange’s Multipliers and Charpit Method, Solution of linear PDE with constant coefficients, Solution of one dimensional heat and wave equation by method of separation of variables.

Text Books1. R. K. Jain and S. R. K. Iyengar, Advanced Engineering Mathematics, Narosa Publications.

ISBN: 9788184875607.2. G. F. Simmons and Differential Equations with Applications and Historical Note, McGraw Hill.

ISBN: 0070530718.3. D. G. Zill and P. D. Shanahan , A first course in complex analysis with applications, Jones and

Bartlett Publishers. ISBN: 9789380108193.4. M. D. Raisinghania, Ordinary and Partial Differential Equations, S. Chand Publishers. ISBN:

9789385676161.

Reference Books1. M. D. Greenberg, Advanced Engineering Mathematics, Pearson Education, India.

ISBN: 9788177585469.2. I. Sneddon, Elements of Partial Differential Equations, McGraw-Hill Book Company.3. R. V. Churchill, Complex Variables and Applications, McGraw Hill. ISBN: 9780070108530.



Class Tests MSE ESE

Weightage (%) 15 15 20 50


CO/PO PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 PO12 PSO1 PSO2CO1 3 2 0 0 2 0 0 0 0 0 0 0 0 0CO2 3 2 0 0 2 0 0 0 0 0 0 0 0 0CO3 3 2 0 0 2 0 0 0 0 0 0 0 0 0CO4 3 2 0 0 2 0 0 0 0 0 0 0 0 0CO5 3 2 0 0 2 0 0 0 0 0 0 0 0 0CO6 3 2 0 0 2 0 0 0 0 0 0 0 0 0Average 3 2 0 0 2 0 0 0 0 0 0 0 0 0


MECH 2012 STRENGTH OF MATERIALS L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure Basic Knowledge of laws of Physics.

Basic Knowledge of Mathematics.Basic knowledge of Engineering Mechanics

Co-requisites --

COURSE OBJECTIVES1. To help the students learn how to apply their analytical and mathematical

skills for problems involving different loadings and conditions.2. To enable students prepare clear and understandable diagrams,

mathematical model. 3. To help students develop the ability to analyse and model real life problems

involving constant or variable loading. 4. To enable students acquire skills for designing and improving various

mechanical systems for their profession.

COURSE OUTCOMES On completion of this course, the students will be able to,CO1. Understand the basic principles of stress and strain in solid bodies.

CO2. Apply stress-strain relationships in single and compound members subjected to different types of loading such as tension, compression, shear, bending, torsion etc.CO3. Analyze Engineering problems using basic principles of stress and strain.CO4. Evaluate failure of structural and mechanical components under various loading conditions.

CATALOG DESCRIPTIONMechanics of materials is also called ‘strength of materials’. The scope of the subject is very vast. The subject provides understanding of basic as well as advanced concepts of stress and strain distribution in components as tiny as a paper pin to as large as the shaft of turbine of a mega power plant. This subject deals with the behavior of solid (rigid bodies as well as deformable bodies) objects under various loadings. The subject helps in understanding the distribution of stresses and strains under various loadings and different conditions. The external force on a mechanical component can be of various types such as axial forces of type, tensile as well as compressive, shear force, bending moment, torsion or forces developing due to temperature difference. The subject starts with stress and strain distribution for axial and shear loads. Thermal stresses, strains are also considered. The stresses/ strains in composite shafts, beams as well as statically indeterminate beams are studied. In next unit distribution of shear force and bending moment is considered for various beams and loads/loads distributions. Point of contra-flexure, point of maximum shear and point of maximum bending moment are some important points which can be found after studying this unit. In fourth unit stresses due to bending are studied. Positive bending, negative bending, shape of beams after these and nature as well as magnitudes of the bending stresses are learnt in this unit. In fifth unit torsion and its effect is studied in solid, hollow and composite shafts. How the shear force varies across the cross section of a shaft, how angle of twist varies with torque/ diameter of the shaft is studied in this unit. Then next unit concerns about the stresses and strain in thin pressure vessels. The pressure vessels studied include cylindrical as well as spherical shells. We try to find tangential and axial stresses due to an internal pressure. Corresponding tangential and axial strains are also determined and these are further used in determining the change in diameter, change in length and change in volume of a thin pressure vessel.

The next unit is concerned about the deflection of beams under various types of transverse loads/ load distributions. Various methods of beam deflection and beam slope are studied. After this the behavior of structural columns under compressive loads is studied. Euler’s theory, Rankine theory and Secant formula are learnt. In next unit the complex stresses and strains are studied. This unit concerns about stress/ strain components on an inclined plane. Students get to learn how to determine principal stresses and strains and then this information is further utilized in failure theories for prediction of failures stresses, strains or loads. Last unit is about riveted and welded joints. The strength of riveted and welded joints is determined and the values of forces for which these joints fail are determined.

Course Content UNIT 1: SIMPLE STRESS AND STRAIN I 5 LECTURE

HOURSNormal Stress & Strain, Hooke’s Law, Deformation in Prismatic, Stepped, Linearly Varying cross section & Composite Members Under Axial Load & Self Weight, Stress & Strain in Indeterminate Member

UNIT 2: SIMPLE STRESS & STRAIN II 4 LECTURE HOURSVarious types of stresses and strains, Elastic constants, Temperature stresses, axial force diagrams, Generalized Hook’s Law, Working Stress concept

UNIT 3: SHEAR FORCE AND BENDING MOMENT 5 LECTURE HOURSShear Force and Bending Moment Diagram in Cantilever and Simply Supported & Compound Beam with Concentrated, Distributed Load and Couple, Overhanging Beams, Point of Contra- Flexure, Relation between Shear Force, Bending Moment & Loading

UNIT 4: STRESSES IN BEAMS 4 LECTURE HOURSTheory of Bending, Flexural Formula, Bending & Shear Stresses in Beams, Section Modulus & Moment of Resistance Shear Stress Formula. Shear Stress Determination in Symmetrical Sections.

UNIT 5: TORSION 4 LECTURE HOURS

Introduction, Theory of Torsion, Shear Stresses in Hollow & Circular Shafts due to Torsion, Composite Shafts, Stresses due to Combined Bending and Torque in Shafts, Spring concept

UNIT 6: THIN CYLINDRICAL AND SPHERICAL SHELLS 4 LECTURE HOURSThin Wall Cylinders & Spheres, Stress due to Internal Pressure, Change in Diameter & Volume

UNIT 7: DEFLECTION OF BEAM 5 LECTURE HOURSRelationship between curvature, deflection and slope of a deflected beam. Macaulay’s Method for Slope & Deflection of determinate beams. Double Integration Method for determinate beams, Moment Area Method for Slope & Deflection of determinate beams.

UNIT 8: AXIALLY AND ECCENTRICALLY LOADED COLUMNS 3 LECTURE HOURSIntroduction, Buckling Effect, Euler’s Theory, Rankine’s Formula for Axially Loaded Columns with Different End Conditions, Concept of Equivalent Length, Stresses due to Eccentric loads, Core of Section

UNIT 9: COMPLEX STRESSES 5 LECTURE HOURSStresses on Inclined Plane, Principal Stresses and Strains, Principal planes, Theories of Failure

UNIT 10: RIVETED & WELDED JOINTS 4 LECTURE HOURSTypes of Riveted Joints, Failure of a Rivet, Riveted Joint, Strength of a Rivet Strength, Efficiency and design of a Riveted Joint, Types of Welded joints, Strength and Design of Welded joints.

Text Books:

1. Strength of Materials – U.C. Jindal2. Strength of Materials – S S Rattan3. Strength of Materials – Sadhu Singh4. Mechanics of Materials – B C Punmia

Reference books:1. Mechanics of Materials – Timoshenko2. Mechanics of Materials - Russell C. Hibbler3. Strength of Materials – Ryder

4. Mechanics of Materials – Gere and Goodno


Examination Scheme:



PO/COPO1

PO2PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

CO1 3 2 0 0 0 0 2 0 0 0 0 1 0 1

CO2 3 3 1 0 0 0 0 0 0 0 0 1 0 1

CO3 3 3 2 1 0 0 0 0 0 0 0 1 0 1

CO4 3 3 2 3 2 0 2 0 0 0 0 1 2 1

Average

32.75

1.6 2 2 0 2 0 0 0 0 1 2 1


MECH 2002 Applied Fluid Mechanics L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure Basic knowledge of physics and mathematics (Trigonometry and

Calculus), Basic knowledge of Thermodynamics (Ist law)

Co-requisites --

COURSE OBJECTIVES1. To help the students understand the fundamentals and relevance of fluid

mechanics in the broader context of engineering sciences in general, and automotive engineering in particular

2. To enable students to understand fluid properties and apply laws of fluid mechanics and analyse fluid flows through different configurations along with the measurement of flow parameters.

3. To empower students with the expertise of experimentation, simulation and the fundamental concepts that are required to translate a novel engineering idea to reality through dimensional analysis and similitude.

4. To expose students to a wide variety of research areas and concerns in and around fluid mechanics such as energy, health etc. across multidisciplinary domains.

5. To equip students with necessary engineering skills such as solving engineering problems in a professional way, using commercial software packages such as MATLAB for data analysis and presentation, numerical simulations etc.

COURSE OUTCOMES CO1. Apply laws of fluid mechanics to calculate forces on submerged surfaces CO2. Compute kinematics properties of a fluid elementCO3. Understand and formulate the governing equationsCO4. Apply conservation laws to fluid flow problems in engineering applications.CO5. Apply boundary layer concepts on various geometries.

CATALOG DESCRIPTIONFluid flows are important in many scientific and technological problems including automotive design, atmospheric and oceanic circulation, renewable energy generation, energy production by chemical or nuclear combustion in engines and

stars, energy utilization in vehicles, buildings and industrial processes, and biological processes such as the flow of blood. The highly multidisciplinary nature of the subject can be gauged from the fact that it is taught across multiple disciplines ranging from Mechanical, Aerospace, Civil, Chemical to Environmental Engineering. The current course covers the fundamental background in the statics and dynamics of fluids, with a special emphasis on applications of fluid mechanics, as relevant to engineering sciences in general and automotive engineering in particular. The course begins with a description of different fluid properties and covers the basic conservation laws of mass, momentum and energy. The students will learn the fundamental laws of fluid dynamics and then apply it to two distinct type of flows commonly found in real life: internal flows and external flows. The students will thus get an adequate exposure to internal flows such as pipe flows in industry, or external flows viz. flow over an aircraft wing. The student will also learn the art of engineering approximations, and the fundamental concepts of dimensional analysis, similitude and experimentation, that are involved in translating a novel idea to a real-world application. Further, being a rigorous course on problem-solving, it will acquaint students with engineering problem-solving approaches and the effective use of commercial software packages to answer engineering questions.

Course Content UNIT 1: INTRODUCTION 10 LECTURE

HOURSFundamentals about Fluid. Classification of fluids. Physical properties of fluids, i.e., Viscosity, Compressibility, Surface Tension and Capillarity; Fluid Statics: Pascal’s law; Pressure-density-height relationship. Measurement of pressure by Manometers and mechanical gauges. Pressure on plane and curved surfaces. The Hydrostatic law; Total Pressure and Centre of pressure; Buoyancy. Stability of immersed and floating bodies. Fluid masses subjected to uniform horizontal and vertical acceleration.

UNIT 2: FLUID KINEMATICS: 9 LECTURE HOURSDescription of fluid flow: Lagrangian and Eulerian approach; Types of fluid Flows: Steady and unsteady, Uniform and non-uniform, Laminar and turbulent flows, Stream lines, Differential and Integral form of Continuity equation; Rotation, Vorticity and Circulation; Elementary explanation of Stream function and Velocity potential. Introduction to Navier-Stokes Equations. Euler’s equation of motion along a streamline and its integration. Bernoulli’s equation and its applications, Pitot tube.

Flow through orifices, Mouthpieces, Nozzles. Notches, Weirs, Free and Forced vortex motion.

UNIT 3: 9 LECTURE HOURSImpulse-Momentum Principle; Moment of momentum equation; Laminar Flow: Equation of motion for laminar flow through pipes; Flow between parallel plates. Kinetic energy and Momentum correction factors. Momentum correction factors, Stokes law. Flow through pipes; Flow between parallel plates.

UNIT 4: 12 LECTURE HOURSBoundary Layer Analysis: Boundary layer thicknesses; Boundary layer over a flat plate. Laminar boundary layer; Application of Von-Karman Integral Momentum Equation. Turbulent boundary layer; Laminar sub-layer; Local and average friction coefficient; Total drag, Boundary layer separation and its control. Flow Through Pipes: Nature of turbulent flow in pipes; Equation for velocity distribution over smooth and rough surfaces; Major and Minor energy losses; Hydraulic gradient and total energy lines; Flow in sudden expansion, contraction, Concept of equivalent length; Branched pipes; Pipes in series and parallel configurations.

UNIT 5: 3 LECTURE HOURSFlow Past Submerged Bodies: Drag and lift, Types of drag force. Drag on sphere, Cylinder and airfoil, Circulation and Lift on a cylinder and airfoil; Magnus effect.

Text Books

1. Som, S C and Biswas, G. “Introduction to fluid mechanics and Fluid Machines” McGraw Hill Publishing Company, New Delhi

2. Young, D. F., Munson, B. R., Okiishi, T. H., & Huebsch, W. W. (2010). A brief introduction to fluid mechanics. John Wiley & Sons.

3. Kumar, D. S. (2015). Fluid Mechanics and Fluid Power Engineering. Katson BooksReference Books

3. Cengel and Cimbala's Fluid Mechanics Fundamentals and Applications, McGraw Hill Publishing Company, New Delhi

4. Douglas, J. F.; Gasiorek, J. M. and Swaffield, J. A. Fluid Mechanics, Pearson Education5. Fox, R. W., McDonald, A. T., & Pritchard, P. J. (1998). Introduction to fluid mechanics

(Vol. 5). New York: John Wiley & Sons.6. F. M. White, Fluid Mechanics, McGraw-Hill, 3rd ed., 1993.7. Modi, P N and Seth, S M “Hydraulics and fluid Machines” Standard Book House, New

DelhiModes of Evaluation: Quiz/Assignment/ presentation/ extempore/ Written Examination

Examination Scheme:



PO/CO PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO 11

PO12

PSO1

PSO2

CO1 2 0 0 0 0 0 0 0 0 0 0 1 0 1CO2 3 0 3 0 3 0 0 0 0 2 0 0 0 0CO3 3 0 0 0 3 0 0 0 0 0 0 2 0 2CO4 3 0 0 0 3 0 0 0 0 0 0 0 2 0CO5 3 0 0 0 3 0 0 0 0 0 2 0 0 2

Average 2.8 0 3 0 3 0 0 0 0 2 2 1.5 2 1.7

1=Weakly mapped, 2= Moderately mapped, 3=Strongly mapped

MEPD 2002 THERMODYNAMICS & HEAT ENGINES

L T P C

Version 1.0 3 1 0 4Pre-requisites/Exposure Basic knowledge of physics and mathematics (Trigonometry

and Calculus)Co-requisites --

COURSE OBJECTIVES1. To help the students understand the fundamentals and relevance of

thermodynamics in the broader context of engineering sciences in general, and aerospace engineering in particular.

2. To be able to use the laws of thermodynamics to estimate the potential for thermo-mechanical energy conversion in aerospace power and propulsion system.

3. To empower students with the expertise of experimentation, simulation and the fundamental concepts that is required to translate a novel engineering idea to reality through thermodynamic relations and power cycles.

4. To expose students to a wide variety of research areas and concerns in and around thermodynamics.

COURSE OUTCOMES On completion of this course, the students will be able to

CO1. Comprehend the thermodynamic systems, properties and laws of thermodynamics.CO2. Apply laws of thermodynamics to flow and non-flow processes. CO3. Analyze the performance of various thermodynamic systems and cycles.CO4. Evaluate various thermodynamic systems.

CATALOG DESCRIPTIONThermodynamics is important in many scientific and technological problems and can be applied to any discipline, technology, applications or the processes. Thermodynamic is used to understand many energy exchanges accompanying a wide range of mechanical and chemical processes. In thermodynamic we study mainly interactions between the thermodynamic system and surrounding in the form of heat and work. Due to interaction between system and surrounding properties of the system will change and we can study all qualitative and quantitative changes within the system by laws of thermodynamics.

Course Content UNIT 1: THERMODYNAMICS PROCESS 8 LECTURE

HOURSSI Units, Systems & Surroundings, Thermodynamic Equilibrium, Properties, State, Path, Process, Cyclic Process, Quasi-Static Process, Reversible and Irreversible Process, Energy Forms, Work and Heat, NTP and STP.

UNIT 2: IDEAL AND REAL GASES 8 LECTURE HOURSEquation of State, Gases and Gas Mixtures, Enthalpy and Specific Heat, Non Ideal Behavior, Super Compressibility Factor.

UNIT 3: LAWS OF THERMODYNAMICS 9 LECTURE HOURSZeroth Law, Temperature and Temperature Scale First Law, Flow Process and Control Volume, Energy Equation, Mechanical Work In Flow Process, Throttling Process, Application To Open System Second Law, Statement, Available and Unavailable Energy Heat Entropy Change for Ideal Gases.

UNIT 4: STEAM 8 LECTURE HOURSProperties, Mollier Diagram, Closed and Open System, Processes, Dryness Factor, Throttling Calorimeter, Rankine Cycle.

UNIT 5: THERMODYNAMIC CYCLES 9 LECTURE HOURSAir Standard Cycles, Otto and Diesel Cycles, Principles of Working of Two and Four Stroke SI and CI Engines.

Text Books1. Engineering Thermodynamics by P.K.Nag, Tata Mc Graw Hill Pub.

2. Engineering Thermodynamics by C.P. Arora.

Reference Books1. Engineering Thermodynamics by Jones and Dugans, PHI Learning Pvt. Ltd.

2. Fundamentals of Thermodynamics by Sonntag, Wiley India Pvt. Ltd.

3. Fundamentals of Classical Thermodynamics by Van Wylen, John wiley & sons.

4. Thermodynamics by J.P. Holman, McGraw Hill.


Examination Scheme:



POs & PSOs

/COs

PO1

PO2

PO3 PO4 PO5 PO6 PO7 PO8 PO9PO1

0PO1

1PO1

2

PSO1

PSO2

CO1 3 2 0 0 0 0 2 0 0 0 0 1 0 0

CO2 3 3 1 0 0 0 0 0 0 0 0 1 1 0

CO3 3 3 2 1 0 0 0 0 0 0 0 1 2 0

CO4 3 3 2 3 2 0 2 0 0 0 0 1 2 0

Average

3 2.75

1.67

2 2 0 2 0 0 0 0 1 1.67 0


MECH 2013 Theory of Machines L T P CVersion 1.0 3 0 0 3Pre-requisites/Exposure a. Basic Knowledge of laws of Physics.

b. Basic Knowledge of Mathematics.c. Basic knowledge of Engineering Mechanics.

Co-requisites --

COURSE OBJECTIVES1. To help the students to understand the basic concept of mechanism and

machines in the broader context of engineering and use of mechanisms to transmit motion and power.

2. To enable the students to understand the basic concept of friction and its application in different engineering problems.

3. To empower the students with the expertise of theoretical and practical knowledge of Gyroscope, Governors and Balancing and their application in industry.

4. To enable the students to apply the knowledge of link motion to solve different engineering problems.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Understand the kinematics and dynamics of different mechanisms and drives. CO2. Apply the concepts of position, velocity and acceleration analyses for various mechanisms. CO3. Analyze problems related to kinematic behaviour and dynamic behaviour of drives, mechanisms and machines. CO4. Evaluate the characteristics of various drives.

CATALOG DESCRIPTIONMechanisms and Machines have considerable fascination for most students of engineering as the theoretical principles involved have immediate applications to practical problems. The main objective of this course is to give a clear understanding of the concepts underlying engineering design. The course involves the kinematics and dynamics of machines. The focus is to empower the students with the theoretical and practical knowledge of mechanisms and machines to enable them to solve complex engineering problems.

Course Content UNIT 1: LINKS AND MECHANISMS 7 LECTURE

HOURSLink types, Kinematic pairs – classification, Constraints and their types, Degree of freedom, Grubler’s equation, Linkage mechanism, Inversions of a four bar mechanism, Inversions of a slider crank mechanism and double slider crank mechanism.

UNIT 2: VELOCITY AND ACCELERATION 7 LECTURE HOURSVelocity and acceleration diagram basic mechanisms, Instantaneous center of rotation, Body center, Simple problems of velocity diagrams on slider crank and four bar mechanisms (Relative velocity method and Instantaneous center of rotation methods), Acceleration diagrams, Klein’s construction, Coriolis component of acceleration.

UNIT 3: FRICTION 8 LECTURE HOURSTypes and laws of friction, Inclined Plane, Efficiency of inclined plane and Vee threads, Screw Jack, Bearings – Collar, Flat pivot, Conical pivot and conical thrust bearings, Clutches – Disk clutch, Cone clutch. Determination of number and size of plates and collars, Theory of lubrication, Friction circle, Friction axis of a link.

UNIT 4: GYROSCOPE & GOVERNORS 6 LECTURE HOURSGyroscope: Principles and applications.Governors: Types of governors: Watt governor, Porter governor, Proell governor, Definitions of sensitiveness, Hunting of governors and Power controlling.

UNIT 5: BALANCING OF MACHINES 4 LECTURE HOURSStatic and Dynamic balancing of rotating masses.

UNIT 6: LINK MOTION 4 LECTURE HOURSLinkage system for elevator, Aileron rudder, Push and pull system, Cable system, spring device, Wire and cables, Fairleads, Turn buckles.

Text Books1. Rattan, S. S. (2014) “Theory of Machines” Fourth Edition, McGraw Hill Education

(India) Private Limited, New Delhi, ISBN 978-93-5134-347-9, 93-5134-347-2

Reference Books1. Uicker, J. J., Pennock, G. R. and Shigley, J. E. (2016) “Theory of Machines &

Mechanisms” Fifth Edition, Oxford University Press, ISBN 0190264489, 9780190264482

2. Bevan, T. (2010) “The Theory of Machines” Third Edition, Pearson Education Limited, ISBN 978-81-317-2965-6.

3. Myszka, D. H. (2012) “Machines and Mechanisms: Applied Kinematic Analysis” Fourth Edition, Pearson Education International, ISBN 0132729733, 9780132729734

4. Martin, G. H. (2002) “Kinematics and Dynamics of Machines” Second Edition, Waveland Press Inc., ISBN 1-57766-250-4, 978-1-57766-250-1.

5. Norton, R. L. (2009) “Kinematics and Dynamics of Machinery” SIE, Tata McGraw-Hill Publishing Company Limited, New Delhi, ISBN 978-0-07-014480-4, 0-07-014480-X.




PO/CO


CO1 3 3 0 0 0 0 0 0 0 1 1 0 0 0CO2 3 3 0 0 0 0 0 0 0 1 1 0 0 0CO3 3 3 0 0 0 0 0 0 0 1 1 0 0 0CO4 3 3 0 0 0 0 0 0 0 1 1 0 0 0Average

3 3 0 0 0 0 0 0 0 1 1 0 0 0


ASEG 2001 Introduction to Aerospace and Avionics Engineering

L T P C

Version 1.0 3 0 0 3Pre-requisites/Exposure Basic knowledge of physics and mathematicsCo-requisites --

COURSE OBJECTIVES1. To introduce to students the fundamental concept of Aerospace Engineering

and its various systems and subsystems.2. To understand the fundamentals and relevance of Aerodynamic forces and

moments in the broader context of engineering sciences in general, and Aerospace engineering in particular.

3. To enable students to understand theory of flight, apply laws of physics, and analyse aerofoils through different aerofoil configurations along with the calculation of aerodynamics parameters.

4. To expose students to different components of aircraft such as Wing, Engine, landing gears, etc. across all the aeronautical engineering domains.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Appreciate the historical developments in the field of aeronautics and astronautics. CO2. Understand the basic mechanism behind lift and drag produced by wings of various sections and planforms.CO3.Classify and Analyze various propulsion systems used by aircrafts and spacecraft.CO4. Estimate various loads and stresses on aircraft structural components.CO5. Recognize and appraise various aircraft and avionics systems.

CATALOG DESCRIPTIONThis is the first course for Aerospace engineering which is a based on basic engineering concepts and system engineering. Historical development are very important aspect to inculcate the level of interest in Aerospace Engineering. Basic understanding of airfoils as well as overall aircraft structure are equally important aspects of aerospace engineering. Finally, knowledge of aircraft auxiliary systems such as hydraulic systems and avionics, etc. are also important for overall aircraft flight.

The course begins with a historical perspective of developments that took place in aviation. The students will learn the fundamental laws of flight theory and then working principle of aircraft propulsion systems. The students will thus get an adequate exposure to the techniques used to estimate aircraft basic aerodynamics through theoretical methods. The student will also learn the art of engineering approximations, and the fundamental concepts of aeronautical engineering, that are involved in translating a novel idea to a real-world application. Further, it will acquaint students with knowledge of working principle of aircraft components to answer basic aerospace engineering questions.

Course Content UNIT 1: INTRODUCTION TO FLIGHT VEHICLES: 8 LECTURE

HOURSClassification of Flight Vehicles along with prominent features of Design; Airplanes, Hovercraft, Helicopter & other V/STOL Machines along with examples, Space vehicles; different concept and configurations from sputnik to Apollo, reusable vehicle; space shuttle and its features. DGCA, Airworthiness Requirements and Air regulations.

UNIT 2: PRINCIPLES OF FLIGHT MECHANICS: 6 LECTURE HOURSLifting & Non Lifting Surfaces. Lift & Drag of Airfoils, Stalling, Finite Span Wing, Induced Drag. Wing Planform Variations, Forward & Aft Swept Wings, High Coefficient of Lift Devices, use of Control Surfaces, Elementary Ideas about Stability & Control of Airplanes. Hovercraft, Helicopter & Space Vehicles Systems.

UNIT 3: PRINCIPLES OF AEROSPACE PROPULSIONS: 8 LECTURE HOURSClassification of Propulsive Units & their features; Fixed & Variable Pitch Air Screws, Piston Prop Engine, Turbo Prop Engine, Turbo Jet Engines & its Variations, Ramjet, Pulse Jet, Rockets Engines; Solid & liquid Propellant Engine, the concept of Staging of Rockets. Structural features in each case selection of Materials. Engine Starting-Systems.

UNIT 4: AEROSPACE VEHICLE STRUCTURE: 6 LECTURE HOURSImportance of Strength/Weight Ratio, Introduction to Loads on different parts of the Vehicle, detailed description of the Fuselage, Wing & Tail Surfaces, Wing Surfaces, Wing Fuselage Jointing Methods, different types of Under Carriages, Structural Design Philosophy of Manned & Unmanned Space Vehicles.

UNIT 5: AIRCRAFT SYSTEMS AND AVIONICS: 8 LECTURE HOURSAviation Electronics description, Data buses. EMR & Frequency band study for satellite and aircraft communication. Basics of navigation and its type. RADAR System: Basic block diagram, Study of Satellites and its basic description.Need for Pressurizing the Cabin, Pressuring System, Oxygen Arrangements, Air Conditioning System, Control of Temperature Integrated Air Conditioning System. Hydraulic System: details & various components, Selector & Sequence, Switches, Electro-Hydro-Mechanical System, Pneumatic System, Auto Pilot System

Text Books1. J. D. Anderson, Introduction to Flight, 8th Edition, 20152. A. C. Kermode, Flight without Formulae, Pitman Publishing; 4th revised edition, 1970

Reference Books

1. McCormick, B. W.; Aerodynamics, Aeronautics, and Flight Mechanics, John Wiley & Sons, Inc.1995

2. Clancy, L. J. ; Aerodynamics: Sterling Book House, 2006




PO/CO PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

CO1 1 1 1 0 0 1 0 0 0 0 0 1 2 1CO2 1 1 1 0 0 1 0 0 0 0 0 1 2 1CO3 1 1 1 0 0 1 0 0 0 0 0 1 2 1CO4 1 1 1 0 0 1 0 0 0 0 0 1 2 1CO5 1 1 1 0 0 1 0 0 0 0 0 1 2 1

Average

1 1 1 0 0 1 0 0 0 0 0 1 2 1

1 = WEEK 2 = MODERATE 3 = STRONG

SEMESTER IV

MECH 3001 Design of Machine Elements L T P C

Version 1.0 3 1 0 4

Pre-requisites/Exposure Basic knowledge of physics and mathematics (Trigonometry), Basic knowledge of Engineering Mechanics.

Co-requisites --

COURSE OBJECTIVES1. To help the students understand the fundamentals and relevance of Machine

Design in the broader context of engineering sciences in general, and automotive engineering in particular

2. To enable students to understand material properties and apply the concepts of engineering mechanics & strength of material and failure analysis of the machine elements.

3. To empower students with the expertise of experimentation, simulation and the fundamental concepts those are required to translate a novel engineering idea to reality through design calculation and failure analysis.

4. To expose students to a wide variety of research areas and concerns in and around machine design such as power transmission, safety etc. across multidisciplinary domains.

5. To equip students with necessary engineering skills such as solving engineering problems in a professional way, using commercial software packages such as ANSYS for design analysis and presentation, numerical simulations etc.

COURSE OUTCOMES On completion of this course, the students will be able to:CO1. Identify the different design aspects and considerations & analyze different theory of failure.CO2. Design for static load & Fluctuating load. CO3. Design of Screws, bolts, Welded and riveted connection, Cotters and cotter joints and power screwCO4. Design of shafts (by ASME code), keys, couplings & Gears (Spur & Helical) CO5. Design of rolling and sliding contact bearings

CATALOG DESCRIPTION

Machine design occupies a prominent position in the curriculum of Mechanical Engineering. It consists of applications of scientific principles, technical information and innovative ideas for the development of a new or improved machine. The task of a machine designer has never been easy, since he has to consider a number of factors, which are not always compatible with the present-day technology. In the context of today’s technical and social climate, the designer’s task has become increasingly difficult. Today’s designer is required to account for many factors and considerations that are almost impossible for one individual to be thoroughly conversant. At the same time, he cannot afford to play a role of something like that of a music director. He must have a special competence of his own and a reasonable knowledge of other ‘instruments.’

Course Content

UNIT I: INTRODUCTION TO DESIGN PROCESS 10 LECTURE HOURSDesign Morphology. General Design Considerations: tearing, bearing, shearing, crushing, etc. Design procedure, Standards in design, Selection of preferred sizes, Indian Standards designation of carbon & alloy steels, Mechanical behavior of materials, selection of materials, manufacturing considerations in design. Stress considerations for variable and repeated loads, Theory of Failures. Endurance limit, fatigue. Fits, tolerances, and surface finish, Reliability, FOS and cost effectiveness etc.

UNIT II: DESIGN OF SCREWS 8 LECTURE HOURSDesign of Screws, bolts and bolted joints, Welded and riveted connection, Cotters and cotter joints, pin fasteners knuckle joints. Power Screws: Forms of threads, multiple threads, Trapezoidal threads, Stresses in screws, Design of screw jack.

UNIT III: DESIGN OF SHAFTS, KEYS AND FLEXIBLE COUPLINGS 8 LECTURE HOURSDesign of Shafts as per ASME code, Cause of failure in shafts, Materials for shaft, Stresses in shafts, Design of shafts subjected to twisting moment, bending moment and combined twisting and bending moments, Shafts subjected to fatigue loads, Design for rigidity, Types of keys, splines, Selection of square & flat keys, Strength of sunk key, Couplings- rigid and flexible

UNIT IV: SPUR & HELICAL GEAR DESIGN 8 LECTURE HOURSSpur Gears:- Introduction, Standard Proportions of Gear Systems, Gear Materials, various design considerations, Beam Strength of gear teeth- Lewis Equation, tangential loading, module Calculations, width calculations, Dynamic tooth loads, Spott’s Equation, types of gear tooth failures, Spur Gear construction, Design of shaft for Spur Gears, Design of arms for Spur Gears.Helical Gears:- Introduction, Terms used in Helical Gears, Face width of Helical Gear Formative no. of teeth and minimum no. of teeth to avoid interference and undercutting, Proportion of the Helical Gears, Strength of Helical Gears, Design of Helical Gears.

UNIT V: BEARING SELECTION & DESIGN 8 LECTURE HOURSRolling Contact Bearings: Types, Static and Dynamic load Capacity, Stribeck’s Equation, Concept of equivalent load, Load life Relationship, Selection of bearing from Manufacturer’s Catalogue, Design for variable loads and Speeds, Bearings with Probability of Survival other than 90%, Lubrication and Mounting of bearings, oil Seals and packing used for bearings. Hydro-static & Hydrodynamics bearing design.

Text Books

1. Design of machine elements V.B. bhandari, TMH 2010.2. Machine Design by Dr. P.C.Sharma and Dr. D. K. Agrawal, S.k.Kataria and sons3. Design data hand book by Mahadevan

Reference Books

1. Handbook of gear design, Gitim M.Maitra, TMH 19942. Fundamental of gear design, Remond J drago, Butterworths, 19883. Bearing design in machinery- engineering tribology, Avraham Harnoy, CRC press 20024. PSG design data handbook5. Applied Tribology: Bearing Design and Lubrication By Michael M. Khonsari, E. Richard

Booser, John Wiley and sons6. Couplings and Joints: Design, Selection & Application , Jon R. Mancuso CRC PressA Text

Book of Machine Design Firewall Media By Rajendra Karwa7. Shaft Alignment Handbook, Third Edition , John Piotrowski - 2006

Modes of Evaluation: Quiz/Test/Assignment/ Written Examination

Examination Scheme:

Components IA MSE ESE

http://www.google.co.in/search?safe=vss&hl=en&tbm=bks&tbm=bks&q=inauthor:%22John+Piotrowski%22&sa=X&ei=lcxMU53tMYjArAfVx4CoBg&ved=0CEoQ9AgwBg

http://books.google.co.in/books?id=b2Qsst8UBEYC&pg=PP17&dq=book+flexible+coupling+operation+and+installation&hl=en&sa=X&ei=lcxMU53tMYjArAfVx4CoBg&ved=0CEgQ6AEwBg

http://books.google.co.in/url?client=ca-print-laxmi_firewall_media&format=googleprint&num=0&channel=BTB-ca-print-laxmi_firewall_media+BTB-ISBN:817008833X&q=http://www.laxmipublications.com/servlet/lpgetbiblio%3Fbno%3D000828&usg=AFQjCNGqopIr473-q-_Il8rZ1VKJ96H00A&source=gbs_buy_r

http://books.google.co.in/url?client=ca-google-print&format=googleprint&num=0&channel=BTB-ca-google-print+BTB-ISBN:082479950X&q=http://www.crcpress.com/product/isbn/9780824799502&usg=AFQjCNHTg9LtXg6aAqAfMrfR2VQenT73Rw&source=gbs_buy_r

http://books.google.co.in/books?id=Q1q6MJdg9h4C&pg=PR8&dq=book+flexible+coupling+operation+and+installation&hl=en&sa=X&ei=bcpMU_GnCIP7rAfc3YGQBQ&ved=0CD8Q6AEwBA

Weightage (%)

30 20 50


PO/CO PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO3

CO1 3 3 3 1 1 0 0 0 0 2 2 1 0 2

CO2 3 3 3 2 2 0 0 0 0 2 2 1 0 3

CO3 3 3 3 2 2 0 0 0 0 3 3 1 0 3

CO4 3 3 2 2 2 0 0 0 0 3 3 1 0 3

CO5 3 3 2 2 2 0 0 0 0 3 3 1 0 3

Average 3 3 2.6 1.8 1.8 0 0 0 0 2.6 2.6 1 0 2.8


ASEG 2002 Aerodynamics I L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure knowledge of Fluid MechanicsCo-requisites --

COURSE OBJECTIVES1. To develop an understanding of low speed aerodynamics, potential flow and

an introduction to compressible flows.2. To introduce the concepts of mass, momentum and energy conservation

relating to aerodynamics. 3. To make the student understand the concept of vorticity, irrotationality,

theory of airfoils and wing sections. 4. To introduce the basics of viscous flow.

COURSE OUTCOMES On completion of this course, the students will be able to understand the different types of flows and their properties – its effects.CO1. Classify various fluid flow regimes and measure the flow parameters.CO2. Apply potential flow theory to predict the velocity, pressure, and force distributions on simple aerodynamic bodies.CO3. Solve simplified forms of the Navier-Stokes equations to obtain analytic solutions to selected fluid flow problems.CO4. Analyze the effect of boundary layer and viscous flow on aerodynamics bodies.CO5. Ability to apply principles of gas dynamics to solve compressible flow problems.

CATALOG DESCRIPTIONThis course builds on the student's background in Fluid Mechanics to deal primarily with internal and external flows (low-speed and high speed) relevant to aerospace applications. Students are expected to be able to analyse flows past airfoils, wings which form the basic building blocks of an airplane.Its objective is to present theoretical aerodynamics with basic numerical applications of potential flow over basic configurations, airfoil, fixed and rotating, and over body of revolution. Furthermore, compressibility effects are considered as well as elementary analysis of the boundary layer including boundary layer transition and turbulent layer.

Course Content UNIT 1: INTRODUCTION: 5

LECTURE HOURSContinuum and free molecular flows, inviscid and viscous flows, incompressible and compressible flows. Newtonian and non-Newtonian flows. Pitot static tube, measurement of air-speed, pressure coefficient. Aerodynamic force and moments. Dimensional analysis, non-dimensional parameters, M, Re, Fr etc., flow similarity.

UNIT 2: DESCRIPTION OF FLUID MOTION: 6 LECTURE HOURSLagrangian and Eulerian methods, description of properties in a moving fluid, local and material rate of change. Equation of conservation of mass for control volume, special form of equation of conservation of mass, differential form of equation of conservation of mass. Streamlines, pathlines, streaklines, vorticity and circulation. Laws of vortex motion. Translation, rotation and rate of deformation of fluid particles. Euler's and Navier-Stokes equations. Derivation of Bernoulli’s equation for inviscid and viscous flow fields. Momentum equation and angular momentum equation in integral form.

UNIT 3: INVISCID INCOMPRESSIBLE FLOW: 8 LECTURE HOURSCondition on velocity for incompressible flow. Laplace's equations. Potential function, stream function. Basic elementary flows: uniform flows, source flow, doublet flow and vortex flow. Superimposition of elementary flows. Non-lifting and lifting flow over a circular cylinder, comparison with real flow over circular cylinder. Kutta-Jaukowski theorem, generation of lift.

UNIT 4: INTRODUCTION TO VISCOUS FLOW: 6 LECTURE HOURSQualitative aspects of viscous flows, viscosity and thermal conductivity. Phenomenon of separation. Navier-Stokes equation; viscous flow energy equation. Some exact solutions to Navier-Stokes equations: Couette flow, Poiseuille flow.

UNIT 5: INTRODUCTION TO INCOMPRESSIBLE BOUNDARY LAYER: 5 LECTURE HOURS

BL concept, BL Properties, Derivation of Prandtl's BL Equations, Blasius Solution, Karman's Integral Equation. Turbulent BL over a Plate, Skin Friction Drag, BL Control.

UNIT VI: ELEMENTS OF COMPRESSIBLE FLOW 6 LECTURE HOURS

Compressible Flow Properties: Total Enthalpy, Total Temperature, Temperature and Pressure Ratios as a function of Mach No., Mass Flow Parameter (MFP). Isentropic Area Ratio (A/A*), Velocity-Area variations, 2D Small Amplitude Wave Propagation. Adiabatic Steady Flow Ellipse, description of Flow Regimes. Introduction to Normal and Oblique Shock Waves. Working out solutions through Gas Tables/Charts.

Text Books1. Anderson, John D. “fundamental of Aerodynamics” Tata McGraw Hill Publishing

Company, New Delhi2. Laurence Joseph Clancy. “Aerodynamics” Sterling Book House, Mumbai

Reference Books1. E L Houghton and P W Carpenter. “Aerodynamics for Engineering Students”

Butterworth Heinemann




PO/CO PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 PO12 PS01 PS02CO1 3 1 0 1 0 0 0 0 0 0 0 1 3 0CO2 3 3 0 1 0 0 0 0 0 0 0 1 3 0CO3 3 3 0 1 0 0 0 0 0 0 0 1 3 0CO4 3 3 0 1 0 0 0 0 0 0 0 1 3 0CO5 3 2 0 3 0 0 0 0 0 0 0 1 3 0Average 3 2.4 0 1.4 0 0 0 0 0 0 0 1 3 0


ASEG 2003 Propulsion I L T P CVersion 2.0 3 1 0 4Pre-requisites/Exposure Basic knowledge of physics and mathematics, Basic

knowledge of ThermodynamicsCo-requisites Gas Dynamics

COURSE OBJECTIVES1. To help the students understand the fundamentals of aircraft propulsion and

the various terms in the integral momentum equation and how jet propulsion works

2. To enable students to apply control volume analysis and the integral momentum equation to estimate the forces produced by aerospace propulsion systems

3. To empower students with the expertise of experimentation, simulation and the fundamental concepts that are required to translate a novel engineering idea to reality through dimensional analysis and similitude.

4. To be able to describe the principal design parameters and constraints that set the performance of gas turbine engines, and to apply ideal-cycle analysis to a gas turbine engine to relate thrust and fuel burn to component-level performance parameters and flight conditions

5. To equip students with workings of multistage compressor or turbine, and to be able to use velocity triangles and the Euler Turbine Equation to estimate the performance of a compressor or turbine stage

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Understand the theory behind rotating propellers and estimate their performances.CO2. Appraise the working of internal combustion engines and their performance analysis.CO3. Appreciate different types of aviation fuels and their characteristics.CO4. Categorize the components of gas turbine engines and estimate their efficiencies.

CATALOG DESCRIPTION

The focus of Propulsion course is on the mechanics and thermodynamics of gas turbines and air-breathing propulsion devices. Calculation of thrust, combustion reactions, specific fuel consumption and operating performance for various aircraft engines. Aerothermodynamics of inlets, combustors, nozzles, compressors, turbines for different class of engines. Review of efficiency improvement measures in gas turbine engines, as well as propeller driven aircrafts. Since the analysis developed in the course is similar to the analysis used in engine design in various class of engines like IC engines, Propellers, as well as gas turbine engines. The entire focus of the course is on developing an approach to analyzing the engine as a complete system and design is stressed for not only on-design but more importantly, for off-design performance.

Course Content UNIT 1: PROPELLER 9 LECTURE

HOURSIdeal Momentum Theory and Blade Element Theory and their relative Merits, Numerical Problems on the Performance of Propellers using Propeller Charts, Selection of Propellers, Fixed, Variable and Constant Speed Propellers, Prop-Fan, Material for Propellers, Shrouded Propellers Helicopter rotor in Hovering Performance.

UNIT 2: AIRCRAFT PISTON ENGINES 9 LECTURE HOURSThe Internal Combustion Engine Process, Brief Historical Sketch S.I and C.I. Engines, 4-Stroke and 2-Stroke Engines, Thermodynamics of Engine Analysis, Combustion Process, Air Standard Cycles, Various Type of Arrangements or Multi-Cylinder Aircraft Engines, their Merits and Operational Efficiencies, Intake and Exhaust Manifolds, Cooling and Lubrication Systems, Valve Timing and Arrangements, I.H.P., B.H.P and F.H.P, Engine Performance, Effect of Altitude, Power required and Power available, supercharging, Preliminary Design of Aircraft Piston Engine

UNIT 3: FUELS, COMBUSTION AND FLAME STABILITY 9 LECTURE HOURSLiquid Fuels, Hydrocarbons, Gasoline, Starting Mixtures and Temperatures, Vapor Lock, other Liquid Fuels and Blends, Combustion Knock and Knock Rating, Carburetion and Fuel Injection, Ignition of the Charge, Ignition System, Gas Turbine Fuels, Solid and Liquid Propellants.

UNIT IV: AIRCRAFT GAS TURBINES ENGINES 9 LECTURE HOURSAir-Standard Brayton Cycle, Actual Gas Turbine Engine Cycle, Compressor and Turbine Efficiencies, Compressor Work and Turbine Work, Centrifugal and Axial type of Compressor, their Comparative Action, Relative Merits in Operations, Combustion Chambers: Various Arrangements, Simplex and Duplex Burners.

Text Books1. Hill Philip, Peterson Carl, Mechanics and Thermodynamics of Propulsion, 1992, Addison

Wesly.2. Roy Bhaskar, Aircraft Propulsion, 2008, Elsevier (India).3. El-Sayed Ahmed, Aircraft Propulsion and gas Turbine Engines, 2008, Taylor and

Francis (CRC press).4. S. Farokhi. Aircraft Propulsion. John Wiley & Sons, 2009

Reference Books1. Saravanamuttoo, H.I.H., Rogers G.F.C., Cohen H. Gas Turbine Theory, 2001, Pearson.2. Oates Gordon C; Aerothermodynamics of Aircraft Engine Components, 1985, AIAA

Education Series.3. J L Kererbrock, Aircraft Engine and Gas Turbine, MIT Press, 19914. Kerrebrock, J. L. Aircraft Engines and Gas Turbines. 2nd ed. MIT Press, 19925. Bathie, W. W., Fundamentals of Gas Turbines, 2nd Ed, John Wiley & Sons, 1992.6. Turns, S. R., An Introduction to Combustion, 2nd Ed, McGraw-Hill, 2000.




PO/CO PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 PO12 PSO1 PSO2CO1 3 3 2 2 0 0 0 0 0 0 0 0 3 0CO2 3 3 2 2 0 0 0 0 0 0 0 0 3 1CO3 3 1 0 1 0 0 0 0 0 0 0 0 3 0CO4 3 3 3 2 0 0 0 0 0 0 0 0 3 2Average

3 2.5 2.33 2.33 0 0 0 0 0 0 0 0 3 1.5


https://mitpress.mit.edu/9780262111621

CHCE 2001 Heat Transfer Processes L T P CVersion 1.0 3 0 0 3Pre-requisites/Exposure Basics of physics and mathematicsCo-requisites --

COURSE OBJECTIVESTo develop skills to analyse any system by using physics, mathematics and chemistry principles to analyse the system without thermal equilibrium.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Describe and analyze the conduction heat transfer mode on rectangular, cylindrical and spherical coordinates (1-D, 2-D and 3-D heat transfer).CO2. Analyze and interpret the convection heat transfer mode (natural and forced convection) in the systems.CO3. Explain and analyze the radiation mode of heat transfer and shape factor.CO4. Describe and analyze the heat exchangers, LMTD, and NTU methods. CO5. Describe and analyze the evaporators and evaporation processes.

CATALOG DESCRIPTIONHeat transfer in engineering consists of the transfer of enthalpy (Rate of movement) because of a temperature difference (Difference in potential between two points of movement). Enthalpy is the name for heat energy, to distinguish it from other sorts, such as kinetic energy, pressure energy, useful work. There has to be a temperature difference, or no heat transfer occurs. (If we insist on a change in enthalpy from a cold body to a warm one, we will have to do more work, as in the case of a refrigerator (We are moving up or against the current [defined as natural flow]). This invariably involves some other process, such as mechanical work via outside forces, and cooling by expansion of gases/internal forces, but within the overall activity heat transfer always goes from the warmer to the cooler.) The temperature difference is called the driving force. Other things being equal, a greater temperature difference will give a greater rate of heat transfer. Along with the heat transfer modes, different heat transfer/exchange systems have also been covered in this subject.

Course Content

UNIT 1: BASICS MODES OF HEAT TRANSFER AND CONDUCTION 8 LECTURE HOURSBasic Equation – One Dimensional, Two Dimensional and Three Dimensional. Steady State Conduction in Slab, Cylinder and Sphere. Critical Thickness of Insulation. Finned Surfaces.

UNIT 2: CONVECTION 10 LECTURE HOURSEquation of Motion. Equation of Energy. Solution of Boundary Layer Flow over Flat Plate. Forced Convection Inside Tubes Under Laminar and Turbulent Flow Conditions. Forced Convection over Cylinders and Spheres. Natural convection: Dimensionless Parameters of Natural Convection: Empirical Correlations for Free Convection for Various Shapes. Boiling and Condensation Heat Transfer.

UNIT 3: RADIATION 6 LECTURE HOURSBlack Body Radiation. Concept of Shape Factor. Methods of Determination of Shape Factor. Radiation Exchange in Enclosure with Black Surface.

UNIT 4: HEAT EXCHANGERS 6 LECTURE HOURSBasic Types of Heat Exchangers. Overall Heat Transfer Coefficient, Log Mean Temperature Differences. NTU Methods for Heat Exchanger Analysis.

UNIT 5: EVAPORATORS 6 LECTURE HOURSTypes of Evaporators. Single and Multiple Effect Evaporation. Calculations for Surface Area Requirements.

Text Books

1. J P Holman, S. Bhattacharyya, Heat Transfer, Tata McGraw Hill, tenth edition, 2011.

2. Cengel. and Yunus., Heat and Mass Transfer, 4/e (SI Units), McGraw Hill Education; 4 edition (28 May 2011).

3. B.K. Dutta, Heat Transfer: Principles and Applications, Prentice Hall India Learning Private Limited (2000).

Reference Books

1. Incropera, Dewitt, Bergman and Lavine., “Fundamentals of heat and Mass Transfer”, Prentice Hall of India, 2005.

2. Donald Kern, Process Heat Transfer, McGraw Hill Education; 1 edition (18 October 2001).




PO/CO

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO 11

PO12

PSO1

PSO2

CO1 2 3 1 0 0 0 0 0 0 2 0 0 0 0CO2 3 2 0 1 0 0 0 0 0 2 0 0 0 0CO3 3 2 0 1 0 0 0 0 0 1 0 0 0 0CO4 3 3 2 1 0 0 0 0 0 3 0 0 0 0CO5 2 2 2 0 0 0 0 0 0 2 0 0 0 0

Average 2.6 2.4 1.7 1 0 0 0 0 0 2 0 0 0 0

1=weakly mapped2= moderately mapped3=strongly mapped

LNPS 1013 (online course) Venture Ideation L T P CVersion 0.0 2 0 0 2Pre-requisites/Exposure Needs basic knowledge of entrepreneurshipCo-requisites --

COURSE OBJECTIVES1. To provide knowledge to students pertaining to entrepreneurial process 2. To enable students to understand characteristics of successful entrepreneur

and tools for entrepreneurial ventures. 3. To impart knowledge related with opportunity identification techniques,

entrepreneur prototype and to Evaluate entrepreneurial business models

COURSE OUTCOMES CO1: Assess personal capacity in the context of the entrepreneurial processCO2: Assess characteristics of successful entrepreneurs and entrepreneurial forms and processesCO3: Apply resources, research, and tools for entrepreneurial venturesCO4: Analyze opportunity identification techniquesCO5: Analyze feasibility terminology, processes, models, and techniquesCO6: Analyze tools and methods for planning entrepreneurial venturesCO7: Develop ideation and planning documents for entrepreneurial venture

CATALOG DESCRIPTIONWelcome to Venture Ideation! Just as a farmer plants and cultivates a seed in order to grow a crop, an entrepreneur starts with a seed of an idea and nurtures and develops it to create a viable business. Your interest in pursuing a passion or bringing a vision to reality is driving your entrepreneurial pursuits. But how can you cultivate and grow your idea into a profitable business? Venture Ideation is structured to help you answer this question. You will begin by assessing whether the life of an entrepreneur is the right fit for you. In your assessment, you will examine the entrepreneurial mindset and compare the skills, strengths, and goals of successful entrepreneurs to those of your own. You will continue by exploring methods for identifying opportunities and selecting one opportunity to pursue. After you have selected your opportunity, you will begin the process of evaluating whether your idea can thrive as a viable business. In this process, you will determine the feasibility of your idea by completing technical, market, industry, and financial analyses. You will conclude this course by developing a business model and a timeline for implementing your venture. The guided analyses, models, and timelines that you develop will serve as excellent references for you as you pursue your entrepreneurial interests outside of this course. Throughout this course, you will work with your colleagues to bolster your ideas and gain new perspectives. In some

learning activities, you will work with a small group of your colleagues in order to complete assignments and receive specialized feedback. In addition, you will be encouraged to develop a peer network with your colleagues that you can maintain throughout your career as an entrepreneur. The relationships that you build in this course are to your benefit. Remember, an entrepreneur can never have too many resources! Again, welcome to Venture Ideation!

Course Content UNIT I: DO YOU HAVE IT IN YOU 03 LECTURE

HOURSCreate an entrepreneurial peer network, Assess personal capacity for entrepreneurship, Analyze the impact of self-assessment results on entrepreneurial pursuits, Analyze entrepreneurial forms and processes, Assess characteristics of successful entrepreneurs, Explain differences between self-assessments and characteristics of successful entrepreneurs, Create a personal entrepreneurial action plan

UNIT II: FINDING THE RIGHT OPPORTUNITY FOR YOU 02 LECTURE HOURSApply creative brainstorming techniques, Evaluate entrepreneurial opportunities, Evaluate whether entrepreneurial opportunities align with personal characteristics

UNIT III: WILL YOUR IDEA WORK? 02 LECTURE HOURSCreate an elevator pitch for a product or service, Evaluate technical feasibility of a product or service Develop measures of technical feasibility, Evaluate measures of technical feasibility, Create a prototype for an entrepreneurial opportunity, Evaluate entrepreneurial prototypes, Analyze intellectual property laws applicable to entrepreneurial pursuits

UNIT IV: WHO ARE YOUR CUSTOMERS? 02 LECTURE HOURSApply secondary market research resources to an entrepreneurial opportunity, Apply primary market research techniques for an entrepreneurial opportunity, Analyze market segmentation, targeting, and positioning for an entrepreneurial opportunity, Evaluate the market feasibility for an entrepreneurial opportunity

UNIT V: WHO ARE YOUR COMPETITORS? 03 LECTURE HOURS

Analyze industry factors that influence the feasibility of an opportunity, Assess attractiveness of an industry using an industry analysis model, Evaluate product or service based on industry analysis

UNIT VI: WHAT DO THE NUMBERS TELL YOU? 02 LECTURE HOURSApply revenue-forecasting techniques, Generate a pro forma income statement, Analyze a pro forma income statement for sensitivity, Evaluate income statement outcomes based on personal expectations and needs, Evaluate financial feasibility for potential ventures, Create a personal entrepreneurial action plan

UNIT VII: MORE THAN JUST AN IDEA 02 LECTURE HOURSCreate a business model for an entrepreneurial venture, Create a timeline for venture implementation, Analyze challenges associated with starting an entrepreneurial venture, Evaluate entrepreneurial business models, Create an executive summary for an entrepreneurial venture, Evaluate executive summaries for entrepreneurial ventures, Re-assess personal capacity for entrepreneurship

UNIT VIII: INDIAN PERSPECTIVE 02 LECTURE HOURSEntrepreneurship and Innovation in Indian context, Indian examples and learnings from them, Societal and Economical implications of starting a new business

TEXT BOOKS:

Modes of Evaluation: Quiz/Test/Assignment/Written ExaminationExamination Scheme:



PO/CO

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO 11

PO12

PSO1

PSO2

CO1 0 0 2 0 0 2 0 0 1 1 2 0 0 0CO2 0 0 2 0 0 2 0 0 1 1 2 0 0 0CO3 0 0 2 3 0 2 0 0 1 1 2 0 0 0CO4 0 0 2 0 0 2 0 0 1 1 2 0 0 0

CO5 0 0 2 0 0 2 0 0 1 1 2 0 0 0CO6 0 0 2 0 0 2 0 0 1 1 2 0 0 0CO7 0 0 2 0 0 2 0 0 1 1 2 0 0 0

Average 0 0 2 3 0 2 0 0 1 1 2 0 0 0


SEMESTER V

ASEG 3001 Flight Mechanics I L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure Knowledge of physics and Mechanics, Knowledge of

Introduction of Aerospace EngineeringCo-requisites --

COURSE OBJECTIVES1. To develop an understanding of aircraft flight mechanics.2. Understand lift and drag and wing performance 3. To understand the parameters effecting the performance4. To enable students to the effect of aerodynamic and inertial forces for estimating performance of aircraft.5. Understand performance characteristic of propeller and jet propulsion systems6.To empower students with the expertise and to study the impact of aircraft design characteristics on performance.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Predict the properties of standard atmosphere at various altitudes.CO2. Estimate the drag of an aircraft by applying the knowledge of fluid mechanics andEngineering mechanics.CO3. Analyze the effect of high lift devices on the performance of an aircraft.CO4. Evaluate the performance of an aircraft in steady and level flight. CO5. Evaluate the performance of an aircraft in accelerated flight.

CATALOG DESCRIPTIONThe branch of engineering is to studies the motion of aerospace vehicles in flight when acted upon by gravitational, aerodynamic, propulsive, and other external forces. In this set of lectures we will focus on the flight mechanics of entry and descent vehicles, with an emphasis on: - deriving the necessary differential equations - modeling gravity and aerodynamic forces. Flight mechanics deals with the interaction between vehicles and the atmosphere. Problems in this area include producing more efficient designs, improving the control systems for aircraft, reducing aircraft vibration and noise, etc. The course covers aircraft performance in

drag estimation of complete aircraft, straight and level flight, climb, gliding take-off and, landing, Range and Endurance, turning.

Course Content

UNIT 1: THE STANDARD ATMOSPHERE AND AIRFLOW 4 LECTURE HOURSStandard Atmosphere, relation between Geopotential and Geometric Altitudes, Pressure, Temperature and Density Altitudes. Relation for Stratosphere and Troposphere. Stability of Atmosphere, Aero-Thermodynamics. Measurement of Air-speed: True Airspeed, Indicated Airspeed and Equivalent Airspeed, Airspeed Indicator.

UNIT 2: AERODYNAMIC DRAG 6 LECTURE HOURSCause of Drag, it's effects, Types of Drag and affecting factors. Drag Polar, Compressibility Drag, Design for Minimum Drag, Estimation of Drag of Complete Airplane, Terminal Velocity.

UNIT 3: AERODYNAMIC CHARACTERISTICS 8 LECTURE HOURSForce and Moments Coefficients from Dimensional Analysis. Pressure Distribution over 2D Airfoil, Variation with Angle of Attack, Center of Pressure, Aerodynamic Center, Problems connected with Them. Lift, Drag and Moment Coefficients; Relations between Lift and Drag. Estimation of these characteristics from Measured Pressure Distributions, Variation of Aerodynamic Coefficients with Reynold's Number and Mach number. Effect of Span, Aspect Ratio, Plan Form, Sweep, Taper and Twist on Aerodynamic characteristics of a Lifting Surface. Delta Wing Aerodynamics.

UNIT 4: HIGH LIFT SYSTEMS 4 LECTURE HOURSAirfoil's Maximum Lift Coefficient, Leading and Trailing Edge Devices, Effect of Sweep Back. The deep stall. Effect of Re, Propulsive lift, V/STOL Configurations.

UNIT 5: AIRPLANE PERFORMANCE IN STEADY FLIGHT 9 LECTURE HOURSVariation of Drag with Flight. Speed conditions for Minimum Drag, Minimum Power Conditions; Power at other Speeds. Gliding Flight, Shallow and Steep Angles of Glide; Sinking Speed, Minimum Sinking Speed, Time of Descent. Climbing Flight at Shallow Angles, Correction for Steep Angles, Time to Flight, Maximum Rate of Climb.

UNIT 6: AIRPLANE PERFORMANCE IN ACCELERATED FLIGHT 7 LECTURE HOURS

Take-off and Landing, Calculations of Take-off Ground Run, Take off Distances. Minimum Ground Run, Assisted Take-off, Calculation of Landing Ground Run. Range and Endurance and Problems connected with them.

UNIT 7: MANEUVERS 4 LECTURE HOURSIntroductory Comments on Spins and Stalls; Turning Flight, Maneuvers in 3D space.

Text Books1.Anderson, John D. “Introduction to Flight” Tata McGraw Hill Publishing Company, New Delhi2.Laurence Joseph Clancy. “Aerodynamics” Sterling Book House, Mumbai

Reference Books1.Anderson, John D. “Aircraft Performance and Design” Tata McGraw Hill Publishing Company, New Delhi2.Kermode, A.C., “Mechanics of Flight”, Himalayan Book, 1997Modes of Evaluation: Quiz/Assignment/ presentation/ extempore/ Written ExaminationExamination Scheme:



PO/CO PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

CO1 3 3 0 1 0 0 1 0 1 0 0 0 3 1

CO2 3 3 2 2 0 0 1 0 1 0 0 0 3 1

CO3 3 3 2 2 0 0 1 0 1 0 0 0 3 1

CO4 3 3 2 1 0 0 1 0 1 0 0 0 3 1

CO5 3 3 2 1 0 0 1 0 1 0 0 0 3 1

Average

3 3 2 1.4 0 0 1 0 1 0 0 0 3 1


ASEG 3002 Aircraft Structures L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure Mathematics (Integral and Differential calculus)Co-requisites Engineering Mechanics and Strength of Materials

COURSE OBJECTIVESOn completion of this course, students will demonstrate:

1. Knowledge of modern aerospace structural components;2. Ability to use engineering science tools such as advanced mathematics,

stress analysis.3. Ability to perform stress and deformation analysis on common forms found on

aerospace structures;

COURSE OUTCOMESOn completion of this course, the students will be able toCO1.Describe and apply static equilibrium to 2D and 3D problems.CO2. Analyze various indeterminate structures using analytical methods.CO3. Estimate bending stresses of structural components and their loading pattern.CO4. Calculate shear and torsional stresses on various aircraft structural components.CO5. Appreciate and use modern methods for stress analysis in aircraft structures.

CATALOG DESCRIPTIONThe components of aircraft structures are subjected to forces and deformed elastically during the life of service.This course covers the general information of aircraft structures and materials, and transfer of external aerodynamic loads into structural internal forces. The focus is to deliver the fundamental knowledge for stresses, deflection, and buckling analysis of these structural components under various static loading conditions including torsion, bending and shear.There are two main activities in this course. The first is lectures which emphasize the fundamentals of structural mechanics and analytical approaches for analysis of aircraft structures. The students will learn to derive the theory of linear elasticity and apply it to analyse the components subjected to typical aircraft loading conditions and design requirements.

The second is tutorials which provide a set of lessons and exercises teaching the concepts and methodology in analysis of aircraft structures. The students will be able to learn and understand the procedure of aircraft structural analysis from following tutorial problem solving exercises with group discussions

Course Content UNIT 1: BASIC CONCEPTS OF STRUCTURAL ANALYSIS

8 LECTURE HOURSStress, Strain, Stress-Strain and Thermal relationship in 3D and 2D. Equations of equilibrium, Compatibility, Static and Kinematics Indeterminacy. Energy concepts, Virtual Work. Loads on Aircraft Structural Components, Functions of Different Structural Components. V-n Diagram.

UNIT 2: BENDING, SHEAR AND TORSION OF OPEN AND CLOSED THIN WALLED TUBE 12 LECTURE HOURSBending, Shear and Torsion of open and closed Thin-walled Beam. General Stress, Strain and Displacement Relationship for open and single cell closed section. Structural Idealization, Effect of Idealization on the Analysis of open and closed Section Beams.

UNIT 3: STRESS ANALYSIS OF AIRCRAFT COMPONENTS: 8 LECTURE HOURSWing, Fuselage frame and Wing Ribs. Cutouts in Wings and Fuselage. Landing Gear.

UNIT 4: INTRODUCTION OF MATRIX METHOD IN STRUCTURAL ANALYSIS: 4 LECTURE HOURSIntroduction of Flexible and Stiffness Methods, Choice of Method Stiffness Matrix for an Elastic Spring. Analysis of Pin Jointed Framework, Matrix Analysis of Space Frames, Stiffness Matrix for Uniform Beams.

UNIT 5: INTRODUCTION TO FINITE ELEMENT METHOD IN STRUCTURAL ANALYSIS: 4 LECTURE HOURSIntroduction, Mathematical Idealization of Structure, Application of Finite Element Method. Stiffness Method Concept, Formulation, Formulation Procedures for Element Structural Relationship. Element Shape Function, Simple problem.

Text Books1.T.H.G. MEGSON, (2-12) Aircraft Structures for Engineering Students, Fourth Edition, Butterworth-Heinemann is an imprint of Elsevier, ISBN-13: 978-0-75066-7395, ISBN-10: 0-750-667397

2.E.F. Bruhn, (1973), Analysis and Design of Flight vehicle Structures, Jacobs Pub ISBN13: 9780961523404.

Reference Books1. D. J Perry, J.J.Azar, Aircraft Structures, 2nd Edition, McGraw Hill Publication, ISBN-13:

978-0070491960 ISBN-10: 0070491962. Bruce K. Donaldson, Analysis of Aircraft Structures, 2nd Edition, Cambridge Aerospace

Series, ISBN-10: 0521865832, ISBN-13: 9780521865838.3. J. N. Reddy, An Introduction to the Finite Element Method, McGraw-Hill Mechanical

Engineering, 3rd Edition, ISBN-13: 978-0072466850, ISBN-10: 00724668554. D. V. Hutton, Fundamentals of Finite Element Analysis 1st Edition, McGraw Hill

Publication, ISBN-13: 978-0072922363, ISBN-10: 0072922362.




PO/CO

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO 2

CO1 3 2 1 2 0 0 0 0 0 0 0 0 3 0CO2 3 3 2 3 0 0 0 0 0 0 0 0 3 1CO3 3 3 2 3 0 0 0 0 0 0 0 0 3 1CO4 3 3 2 3 0 0 0 0 0 0 0 0 3 1CO5 3 3 2 3 2 0 0 0 0 0 0 0 3 1Average

3 2.8 1.8 2.8 2 0 0 0 0 0 0 0 3 1


ASEG 3003 Aerodynamics II L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure Basic knowledge of fluid Mechanics, aerodynamics and

engineering mathematicsCo-requisites --

COURSE OBJECTIVES1. To build on the student's background in aerodynamics to deal primarily with

low speed external flows relevant to aerospace applications 2. To present the classical airfoil theories of incompressible aerodynamics that

can be utilized for solving problems in aeronautics and other fields of engineering.

3. To develop an understanding of incompressible three-dimensional wing theory amongst students.

4. To present to the students the empirical relations used in subsonic aerodynamics that may be utilized for conversion of incompressible aerodynamic data to compressible ones.

5. To develop an understanding of the aerodynamic design of subsonic airfoils amongst students.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Apply theory of complex potential function to two-dimensional incompressible irrotational flows. CO2.Estimate the aerodynamic characteristics of two-dimensional airfoils in inviscid, incompressible flow using thin airfoil theory. CO3. Compute the aerodynamic characteristics of a three dimensional wing using finite wing theories.CO4: Analyze the compressibility effect on the aerodynamic coefficients of subsonic airfoils.

CATALOG DESCRIPTIONThe understanding of subsonic and low speed flow over airfoils is fundamental to the design of aeronautical and aerospace vehicles. Besides aerospace engineering, the knowledge of low speed aerodynamics is essential to the design of high-rise buildings, automobiles, and wind turbines as well. This course covers concepts of

subsonic aerodynamics for students of aerospace engineering. The course covers concepts in incompressible airfoil theory, including analysis of symmetric and cambered airfoils using analytical and numerical approaches. The analytical approach includes the mathematical conformal transformation approach and the small perturbation based thin airfoil theory. The course also covers three dimensional wing theory, including down wash, lifting-line theory, elliptic wings, general twisted wings, application of fundamentals to the design of a wing to meet given performance criteria. Both these airfoil and wing theories help students to correlate the aerodynamic coefficients obtained in wind tunnels and motivate the design for better aerodynamic efficiency. Lastly, the course presents the effect of compressibility on the aerodynamic characteristics of airfoils and wings. This helps the students to obtain the aerodynamic coefficients of airfoils in compressible flows from incompressible flow data, available abundantly in the literature or obtained from in-house wind tunnel tests. Apart from theories, the course provides an opportunity to use these theories to obtain state of the art numerical solution to flow over airfoils incompressible flows.

Course Content UNIT 1: CONFORMAL TRANSFORMATION 10

LECTURE HOURSComplex Potential Function, Blasius Theorem, Principles of Conformal Transformation, Kutta - Juokowaski Transformation of a Circle into Flat Plate, Airfoils & Ellipses.

UNIT 2: INCOMPRESSIBLE FLOW OVER AIRFOILS 08 LECTURE HOURSGlauert’s Thin Airfoil Theory, Symmetrical Airfoil, Cambered Airfoil, Flapped Airfoil, Determination of Mean Camber Line Shapes for Uniform & Linear Distribution of Circulation. Description of flow about Multi-Element Airfoils.

UNIT 3: INCOMPRESSIBLE FLOW OVER FINITE WINGS: 10 LECTURE HOURSDownwash & Induced Drag, Biot -Savart’s Law and Helmholtz’s Theorem, Prandtl’s Classical Lifting Line Theory, Fundamental Equations. Elliptic Lift Distribution, General Lift Distribution, Effect of Aspect Ratio, Lifting Surface Theory, Formation Flying, Ground Effect. Flow Field of Delta Wing. Sample Calculation of Lift and Drag on Delta Plan Forms.

UNIT 4: COMPRESSIBLE SUBSONIC FLOWS OVER AIRFOILS: 08 LECTURE HOURSThe Derivation of Velocity Potential Equation. Linearized Velocity Potential Equation. Prandtl - Glauert Compressibility Correction. Critical Mach Number, Whitcomb’s Area Rule, Super critical Airfoil

Text Books1. John D Anderson, Jr., Fundamentals of Aerodynamics, 5th Ed., McGraw Hill, 2005. 2. E. L. Houghton and P.W. Carpenter, Aerodynamics for Engineering Students, 5th Ed.,

Butterworth-Heinemann, 2003.

Reference Books1. Tapan K. Sengupta, Theoretical and Computational Aerodynamics, John Wiley & Sons

Ltd., 2015.2. Joseph Katz and Allen Plotkin, Low Speed Aerodynamics, 2nd Ed., Cambridge University

Press, 2001.Modes of Evaluation: Quiz/Assignment/ presentation/ extempore/ Written Examination:

PO/CO PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 P012 PSO1 PSO2CO1 3 1 0 1 0 0 0 0 0 0 0 1 3 2CO2 3 1 0 1 0 0 0 0 0 0 0 1 3 2CO3 2 0 0 1 0 0 0 0 0 0 0 2 3 3CO4 3 0 0 2 0 0 0 0 0 0 0 2 3 3Average

2.75 0.5 0 1.25 0.75 0 0 0 0 0 0 1.5 3 2.5



ASEG 3005 AIRCRAFT MATERIALS L T P CVersion 1.0 3 0 0 3Pre-requisites/Exposure Basic knowledge of physics, chemistry and material science.Co-requisites --

COURSE OBJECTIVES1. To provide a strong knowledge base of aerospace students in respect of

various important materials used in the manufacture of aircraft including certain salient machining processes that are specific to the aircraft manufacturing.

2. To provide a knowledge relevant to aircraft structures and materials.3. To provide an overview of the composites uses in modern aircraft.4. To provide the design principles of jigs and fixtures, joining and welding

techniques that are used for manufacturing various components and assemblies of aircraft so as to ensure symmetry of the geometric shapes and to obtain accuracy / repeatability in dimensions.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Describe and identify materials for design, development and manufacturing of aircraft and its components. CO2. Evaluate the properties, performance and applicable domain of typical aerospace materials.CO3. Review standardization of Aircraft Materials Crystalline / material micro-structures.CO4. Select the best fabrication processes to meet the design and operation requirements of aircraft structures and components.

CATALOG DESCRIPTIONThis course provides the skills required to assist the design process of aerospace structures and components considering the broad range of engineering materials available. Students will learn both qualitative and quantitative methods of materials selection. Students will also study the main properties, domain of application and fabrication processes of aerospace materials, with a particular emphasis on lightweight alloys and composite materials. Students will investigate the impact of different materials in critical areas pertaining to the operation of aircraft, such as

structural integrity (including prevention methods), airworthiness requirements (including testing and maintenance), sustainability/recyclability issues and cost effectiveness. Furthermore, students will be exposed to state-of-the-art materials topics (e.g., modern materials for aircrafts), and assess pathways for the development of aerospace structures and components with optimized features.

Course Content UNIT 1: INTRODUCTION: 8 LECTURE HOURS

Properties of Flight Vehicle Materials, Importance of Strength / Weight Ration of Materials for Aerospace Vehicles: Structures, Importance of Temperature Variations, Factors affecting choice of Material for different parts of Air Plane. Light Metal Alloys: Aluminum Alloys, Heat Treatment, High Strength and High Corrosion Resistant Alloys, Magnesium Alloys and their Properties, Heat Treatment, Application to Aerospace Vehicle of these Alloys.

UNIT 2: ALLOY STEELS: 5 LECTURE HOURSClassification of Alloy Steels, Effect of Alloying Elements, Carbon Steels V/s Alloys Steels, Corrosion Resistant Steels, Heat Treatment, Corrosion Prevention Methods, Selection and Application of Steel Alloys to Aircraft Manufacture.

UNIT 3: HIGH STRENGTH AND HEAT RESISTANT ALLOYS 5 LECTURE HOURSClassification of Heat Resistant Material & Iron, Nickel and Cobalt Base Alloys, Refractory Materials: Ceramics, Titanium and its Alloys, Properties of Inconel Monal & K–Monal, Nimonic and Super Alloys: Application to Aerospace Vehicle.

UNIT 4: COMPOSITE MATERIALS: 4 LECTURE HOURSTypes, Curing Processes.

UNIT 5: METAL JOINING PROCESSES: 4 LECTURE HOURSWeld Ability, Standard Welding Practices e.g., Gas Welding, Resistance Welding, Welding of Light Alloys, Rivetting.

UNIT 6 : JIGS AND FIXTURES FOR AIRCRAFT: 4 LECTURE HOURSGeneral Design, Method of Location of Cylindrical and Flat Surfaces, Design Principles of Wing Jig, Fuselage Jig and other components.

UNIT 7: TYPES OF MANUFACTURING: 8 LECTURE HOURSIntroduction to Aerospace Manufacturing, General Engineering v/s Aircraft manufacturing, General Methods of Fabrication of Aircraft and Aero Engine Parts.

Machining Processes: Mechanics of Metal Cutting, Cutting Tool Materials, Tuning, Drilling, Reaming Boring, Broaching, Milling, Grinding, Honing and Lapping, Electric Discharge Machining and Electrochemical Machining. Introduction to CNC Machining. Spark Erosion and Powdered Metal Parts.

Text Books1. G.F. Titterton, “Aircraft Materials and Processes”, Himalayan Books, New Delhi2. Lalit Gupta, “Advanced Composite Materials”, Himalayan Books, New Delhi,19983. Jindal UC, Material Sciences & Metallurgy

Reference Books1. Chapman WAJ, “Workshop Technology”, Vol. I, II, III.2. G.B. Ashmead, “Aircraft Production Methods”.




PO/CO

PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO 2


2 1 1 0 0 0 0 0 0 0 0 0 2 0


ASEG-3006 Aircraft Systems and Maintenance L T P C

Version 1.0 3 0 0 3Pre-requisites/Exposure a. Basic Knowledge of Thermodynamics.

b. Good understanding of Automotive.Co-requisites --

COURSE OBJECTIVES1. To help the students to identify components of systems used in aircraft.2. To enable students to understand basic laws and concepts of

thermodynamics.3. To empower students with the expertise of maintenance, overhauling of

aircrafts that are required to translate a novel engineering idea to reality.4. To expose students to detect defects and applications in Aircraft 5. To equip students with necessary engineering skills such as solving

engineering problems related to cycles used in an aircraft.

COURSE OUTCOMES On completion of this course, the students will be able to:CO1 Understand different types of airplane control systemsCO2. Understand about hydraulic, pneumatic, landing gear system CO3. Classify different fuel and lubricating systems of aircraft. CO4. Appraise the cleaning, Inspection, Repair process of Aircraft.

CATALOG DESCRIPTIONCourse work of this subject includes studies of aircraft structures, various internal systems, maintenance and overhauling of an aircraft. Aircraft maintenance is one of the most important activities that aircraft owners should never underestimate. This is a set of activities that include inspection, reformation and repair of an aircraft. As the owner of an aircraft, you need to know every detail about maintenance if you want to save money and avoid failure in your aircraft system. Aircraft maintenance is not only about replacing a part that is already damaged; this is also about cleaning and refueling. This should be done not only to large planes but also to smaller aircrafts. Maintaining your aircraft is done as a compliance with the rules on aircraft ownership. There are different airworthiness authorities in the world whose

job is to make sure that every owner is doing his part in maintaining the safety and good condition of his aircraft. Power plant maintenance familiarizes students with aircraft electrical and engine systems, and general aircraft maintenance coursework explores the field of aviation. Common topics of study include:

1. Airframe inspection of wood, sheet metal and non-metallic structures 2. Pneumatic, hydraulic and landing gear systems 3. Ignition, lubrication and power plant fuel systems4. Engine installation and inspection

Course Content UNIT 1: AIRPLANE CONTROL SYSTEMS 6 LECTURE

HOURSConventional Systems- Power assisted and fully powered flight controls, power actuated systems, Engine control systems, push pull Rod system, Modern control system- Digital fly by wire system, Auto pilot system Active control Technology, communication and Navigation system Instrument Landing system, VOR –CCV Case studies.

UNIT 2: AIRCRAFT SYSTEMS 6 LECTURE HOURSHydraulic Systems- Study of Typical Workable System- components –Hydraulic system controllers, Modes of operation, Pneumatic systems, Advantages- working principle-Typical air pressure system, brake system, Typical Pneumatic power system, components, Landing gear system- classification- shock absorbers-Retractive Mechanism.

UNIT 3: ENGINE SYSTEMS 8 LECTURE HOURSFuel Systems for piston and jet engine- components of Multi Engines. Lubricating Systems for piston and jet Engines- starting and Ignition Systems-Typical example for piston and jet Engines

UNIT 4: AUXILIARY SYSTEM 6 LECTURE HOURSBasic Air cycle Systems –Vapor cycle systems ,Boost –strap Air cycle system , Evaporative Vapor Cycle System, Evaporative Air cycle system, Oxygen system- Fire Protection System, Deicing and anti-icing system

UNIT 5: INTRODUCTION TO AIRCRAFT MAINTENANCE 10 LECTURE HOURSRequirements, Maintenance of Aircraft, its components, systems, subsystems. Types of Maintenance Scheduling, Mandatory Schedules, Inspection of Aircraft and components, Types of Inspection, Repair, Modifications, Reconditioning, Aircraft Assembly, Rigging, Alignment of fixed Surfaces, Flight controls and systems, Balancing , Inspection and Maintenance.

Text Books

1. “Pilot’s Handbook of Aeronautical Knowledge”, Federal Aviation Administration , FAA-H-8083-25B: 2016 Edition

2. “Aircraft systems”, Ian Moir and Allan Seabridge, 3rd Edition John Wiley & Sons Ltd,1992.

Reference Books1. Aircraft Maintenance and Repair”, Kroes, Watkins 6th Edition, 20152. Acceptable Methods ,Techniques and Practices”, Federal Aviation Administration 4




PO/CO PO1 PO2 PO3 PO4

PO5 PO6 PO7 PO8 PO9 PO10

PO11

PO12

PSO1

PSO2


2 1.75 1 1.67 1.75 0 1 0 0 0 0 1 2.25 1


SEMESTER –VI

ASEG 3004 Propulsion II L T P CVersion 2.0 3 1 0 4Pre-requisites/Exposure Basic knowledge of physics and mathematics, Basic knowledge of

ThermodynamicsCo-requisites Propulsion I, Gas Dynamics

COURSE OBJECTIVES1. To help the students understand the fundamentals and jet propulsion and

Analyse Jet Engines and its components.2. To enable students to apply the basic principles of thermodynamic cycles to

Jet engines, understanding of rational behind several types of jet engines. 3. To empower students with the expertise of compressible fluid flows in the

inlets and various components of the jet engine.4. To expose students to a wide variety of research areas and concerns in and

around jet engines and their components; Performance estimation such as individual performance monitoring, health monitoring of the blades, and overall Engine performance estimation.

5. To equip students with necessary combustion physics in combustion chambers to estimate performance analysis of Jet engines and to characterize design principles.

6. To empower students with the understanding of flow characteristics in axial flow compressors, axial flow turbines, which will help them in design and operation of such equipment.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Apply steady one dimensional gas dynamics principles to internal flows.CO2. Understand and analyze the phenomena of shock, Fanno and Rayleigh flow. CO3. Compute inlet, nozzle, and combustion chamber parameters.CO4. Analyze ideal and real engine cycles using thermodynamic principles. CO5. Evaluate axial flow compressor and Turbines operational parameters.

CATALOG DESCRIPTIONJet propulsion is of paramount importance to air transport. In general, the type of propulsion can classified into air breathing propulsion and rocket propulsion. The focus of the present course lies on air breathing jet propulsion. Air breathing propulsion is largely relying on turbomachines independent of propulsion concepts

(propeller, ducted fan, future undusted fans). The reason is to be found in the unprecedented power density as well as reliability of these machines. In other words, modern air transport would not be possible without having turbomachine-powered propulsion devices in place. The present course gives an introduction into (airbreathing) jet propulsion concepts with a clear focus on turbomachinery. This course presents aerospace propulsive devices as systems, with functional requirements and engineering and environmental limitations along with requirements and limitations that constrain design choices. Air breathing are covered, at a level, which enables rational integration of the propulsive system into an overall vehicle design.

Course Content UNIT 1: BASICS, SIMPLE FLOWS: 6 LECTURE

HOURSNozzle Flow, Nozzle Design, Nozzle Operating characteristics for Isentropic Flow, Nozzle Flow and Shock Waves. Nozzle characteristics for some Operational Engines. Rayleigh Flow and Fanno Flow. Effect of Frictional Duct Length in Subsonic Flow and Supersonic Flow, Numerical Problems in 1D Flow.

UNIT 2: SUBSONIC INLETS: 6 LECTURE HOURSPressure Recovery, Inlet Sizing Drag Flow Distortion. Supersonic Inlets: Total and Sonic State Points, A/A* Normal Shock based Internal Compression Inlets, Design Sizing and Performance. Exhaust Nozzle, C-D Nozzle, Engine Back Pressure Control, Exit Area Ratio, Exhaust Nozzle System Performance in details. Combustion Systems, Burners, Ignition, Flame Stability. After Burners: System Design, Flame Stability, Pressure Losses etc.

UNIT 3: PARAMETRIC CYCLE ANALYSIS FOR IDEAL ENGINE: 6 LECTURE HOURSSteps of Engine Parametric Cycle Analysis, Basic Assumptions. Applications to

Ideal Ramjet Ideal Turbojet with and without afterburner Ideal Turbofan engine, optimum BPR and afterburning Ideal Turnoprop engine, and Ideal Turboshaft engine.

Cycle Analysis of Turbojet, Turbojet with after Burner, Turbofan and Turboprop.

UNIT 4: PARAMETRIC CYCLE ANALYSIS FOR REAL ENGINE: 6 LECTURE HOURS Euler’s Turbo Machinery Equations. Axial Flow Compressor Analysis, Cascade Action, Flow Field. Euler’s Equation, Velocity Diagrams, Flow Annulus Area Stage Parameters. Degree of Reaction, Cascade Airfoil Nomenclature and Loss Coefficient, Diffusion Factor, Stage Loading and Flow Coefficient, Stage Pressure Ratio, Blade Mach No., Repeating Stage, Repeating Row, Mean Line Design. Flow Path Dimensions, No. of Blades Per Stage. Radial Variation, Design Process, Performance.

UNIT 5: AXIAL FLOW COMPRESSOR: 6 LECTURE HOURSEuler’s Turbo Machinery Equations, Axial Flow Compressor Analysis, Cascade Action, Flow Field. Euler’s Equation, Velocity Diagrams, Flow Annulus Area Stage Parameters. Degree of Reaction, Cascade Airfoil Nomenclature and Loss Coefficient, Diffusion Factor, Stage Loading and Flow Coefficient, Stage Pressure Ratio, Blade Mach No., Repeating Stage, Repeating Row, Mean Line Design, Flow Path Dimensions, No. of Blades Per Stage, Radial Variation, Design Process, Performance.

UNIT 6: AXIAL FLOW TURBINE 6 LECTURE HOURSIntroduction to Turbine Analysis, Mean Radius Stage Calculations, Stage Parameters, Stage Loading and Flow Coefficients Degree of Reaction, Stage Temperature Ratio and Pressure Ratio, Blade Spacing, Radial Variation, Velocity Ratio. Axial Flow Turbine, Stage Flow Path, Dimensional Stage Analysis. Multistage Design; Steps of Design: Single Stage and two Stages. Turbine Performance. Blade Cooling.

Text Books1. Jack D. Mattingly, “Elements of Gas Turbine Propulsion”, TATA Mc Graw-Hill Edition,

Fourth Edition, 20102. Flack, R.D.., “Fundamentals of Jet Propulsion”, Cambridge University Press, 2005.3. Liepmann, H., and A. Roshko. Elements of Gas Dynamics. John Wiley Publishers, 1957.

Reference Books1. Baskharone, E.A., “Principles of Turbomachinery in Air-Breathing Engines”, Cambridge

University Press, 2006.2. Kerrebrock J.L., “Aircraft Engines and Gas Turbines”, MIT Press, 1992.3. Mattingly, J.D., “Elements of Gas Turbine Propulsion”, McGraw-Hill Inc., 1996.4. Anderson, J.D., “Modern Compressible Flow: With Historical Perspective”,

McGrawHill, 2002.5. Zuker, R.D., and Biblarz, O.,”Fundamentals of Gas Dynamics”, John Wiley & Sons Inc.,

2002.6. Liepmann, H., and A. Roshko. Elements of Gas Dynamics. John Wiley Publishers, 1957.


Examination Scheme:


Relationship between the Program Outcomes (POs), Program Specific Outcomes (PSOs) and Course Outcomes (COs)PO/CO PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 PO12 PSO1 PSO2CO1 3 2 0 0 1 0 0 0 0 0 0 0 3 0CO2 2 3 0 0 0 0 0 0 0 0 0 0 3 0CO3 3 3 2 0 0 0 2 0 0 0 0 0 2 2CO4 3 2 1 0 0 0 0 0 0 0 0 0 3 2CO5 3 3 3 0 1 0 0 0 0 0 0 0 3 1Average

2.8 2.8 2 0 1 0 2 0 0 0 0 0 2.8 1.67


MATH 2002 APPLIED NUMERICAL METHODS L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure Mathematics up to B.Tech 3rd semester

Co-requisites -- COURSE OBJECTIVES

1. To make the students realize the importance of numerical methods. 2. To enable students to understand the mechanism of iterative techniques. 3. To enable students derive appropriate numerical methods to solve a linear system of equations. 4. To make the students able to solve ODEs and PDEs numerically.


1. Implement iterative and non-iterative numerical methods for the solution of single variable algebraic and transcendental equations by understanding the concept of errors.

2. Interpolate and extrapolate values of the dependent variable from equally and unequally spaced data.

3. Perform numerical differentiation and integration from the available discrete data.

4. Solve the system of linear algebraic equations both by direct and iterative methods.

5. Apply single, multistep and finite difference techniques for the solution of initial and boundary value problems in ODEs.

6. Apply finite difference technique for the solution of PDEs.

CATALOG DESCRIPTIONNumerical methods deal with the study of algorithms that use numerical approximation for the problems arising in science and engineering. The course is aimed to provide the knowledge of numerical methods for solving a variety of mathematical models. It deals with the basic definitions, properties of various finite difference operators and their applications to engineering problems associated with polynomial interpolation, differentiation and integration from the given tabular data. It discusses various algorithms associated with the technique of finding zeros of the algebraic and transcendental equations. This course also provides a detailed

knowledge of various direct and iterative methods to solve system of linear algebraic equations. Several techniques will be discussed for solving initial value problems of ordinary differential equations. The students will also get insight into the solutions of boundary value problems in both ordinary and partial differential equations.

Course Content UNIT I: ERROR ANALYSIS, SOLUTION OF ALGEBRAIC & TRANSCENDENTAL

EQUATIONS (08 LECTURE HOURS)Exact and approximate numbers, rounding off numbers, significant digits, correct digits, various types of errors encountered in computations, propagation of errors, Bisection and Fixed Point Iteration method with convergence criteria, Regula-Falsi and Secant methods with convergence criteria, Newton-Raphson method with convergence criteria

UNIT II: FINITE DIFFERENCE OPERATORS, INTERPOLATION, EXTRAPOLATION, NUMERICAL DIFFERENTIATION

(13 LECTURE HOURS)Introduction to finite difference operators and properties, Factorial notation and Missing term techniques, Newton’s Forward and Backward Interpolation, Gauss’s Forward and Backward Interpolation, Stirling’s and Bessel’s Interpolation, Interpolation of unevenly spaced data by Lagrange’s and Newton’s divided difference formula, Numerical Differentiation

UNIT III: NUMERICAL INTEGRATION, SOLUTIONS OF SIMULTANEOUS LINEAR EQUATIONS & ORDINARY DIFFERENTIAL EQUATIONS (13 LECTURE HOURS)Numerical Integration: Trapezoidal, Simpson’s 1/3 and 3/8 rules with error terms, Composite integral methods: Trapezoidal, Simpson’s 1/3 and 3/8 rules, Gauss Legendre 2-points and 3-points formulae, LU Decomposition, Doolittle, Crouts and Cholesky methods, Gauss Jacobi & Gauss Seidel methods with convergence criteria, Taylor’s series method, Euler’s method, Modified Euler’s method, 2nd and 4th order Runge-Kutta method, Milne Predictor Corrector method

UNIT IV: SOLUTIONS OF ORDINARY AND PARTIAL DIFFERENTIAL EQUATIONS BY FINITE DIFFERENCE METHODS

(8 LECTURE HOURS)Finite difference approximations, Solution of 2 point BVP, Five point finite difference approximations, Liebmann’s Iteration process, Explicit and Implicit methods: Bendre - Schmidt Process, Crank-Nicholson method

Text Books1. M. K. Jain, S. R. K. Iyengar and R. K. Jain, Numerical Methods for Scientific and Engineering

Computation, New Age International, ISBN: 9788122420012.2. S. S. Sastry, Introductory Methods of Numerical Analysis, PHI Learning, India. ISBN:

9788120345928.3. E. Bala Guru Swamy, Numerical Methods, Tata McGraw Hill, India. ISBN: 0074633112.

Reference Books1. F. C. Gerald and P.O. Wheatley, Applied Numerical Analysis, Pearson, India. ISBN:

9788131717400. 2. S. Pal, Numerical methods: Principles, analyses, and algorithms, Oxford University Press, New

Delhi, ISBN: 9780195693751.

Modes of Evaluation: Class tests/Assignment/Tutorial Assessment/Written Examination Examination Scheme:


Class Tests MSE ESE

Weightage (%) 15 15 20 50


CO/PO PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 PO12 PSO1 PSO2CO1 3 2 0 0 2 0 0 0 0 1 0 0 0 0CO2 3 2 0 0 2 0 0 0 0 1 0 0 0 0CO3 3 2 0 0 2 0 0 0 0 1 0 0 0 0CO4 3 2 0 0 2 0 0 0 0 1 0 0 0 0CO5 3 2 0 0 2 0 0 0 0 1 0 0 0 0CO6 3 2 0 0 2 0 0 0 0 1 0 0 0 0Average 3 2 0 0 2 0 0 0 0 1 0 0 0 0


MECH 3012 Introduction to Vibration L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure Basic Knowledge of Kinematics of machinesCo-requisites --

COURSE OBJECTIVES1. Introduce basic aspects of vibrational analysis, considering single degree of

freedom, multi-degree-of-freedom systems and continuous system.2. Discuss the use of exact and approximate methods in the analysis of complex

systems.3. To understand the application of gyroscope and balancing of machines.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Ability to solve different types of single degree and two degree of freedom systems for free vibrations.CO2. Ability to solve different types of single degree of freedom system for forced vibrations.CO3. Ability to understand different applications of vibration and methods to determine natural frequencies.CO4. Understand the different laws and methods for solving multi-degree freedom systems.

CATALOG DESCRIPTIONAn introduction to the theory of vibrations including topics of harmonic motion, resonance, undamped and damped vibrations and harmonic excitation. Multi degree of freedom discrete systems including principal mode, principal coordinates, Rayleigh method, Holzer method and Matrix Iteration Method. Introduction to Virtual Displacement, D’ Alembert’s Principle, Lagrange’s Equation for solving different vibration systems and study of Balancing of machines and gyroscopic effects.

Course Content UNIT 1: SYSTEMS WITH ONE DEGREE OF FREEDOM: 10

LECTURE HOURSDegrees of freedom, Equations of Motion from Energy Method and Newton’s Laws of Motion, General Solution, Steady State Analysis, Rectilinear and Rotational Systems, Application: Free & Forced Vibrations, both undamped and damped

UNIT 2: SYSTEMS WITH TWO DEGREE OF FREEDOM: 8 LECTURE HOURSIntroduction: Undamped Free Vibrations, Principal Modes, Semi-Definitive Systems: A Special Case, Steady State Undamped Forced Vibrations, Damped Free Vibrations, Steady State Forced Vibrations with Damping, Influence Coefficients, Generalized Co-ordinate and Co-ordinate Coupling, Principal Co-ordinates, Orthogonality of Principal Modes of Vibration

UNIT 3: LAGRANGE EQUATION: 3 LECTURE HOURSIntroduction: Simple Exposition, Virtual Displacement, D’ Alembert’s Principle, Lagrange’s Equation, Generalized Forces.

UNIT 4: APPLICATIONS: 3 LECTURE HOURSIntroduction: Equivalent Viscous Damping, Balancing of Machines, Accounting of Gyroscopic Effects.

UNIT 5: DETERMINATION OF NATURAL FREQUENCIES: 4 LECTURE HOURSIntroduction: Rayleigh’s Method, Holzer’s Method

UNIT 6: MULTI-DEGREE OF FREEDOM SYSTEM: 8 LECTURE HOURSMatrix method, Free Vibartions, Principal Modes, Normal Co-ordinates, Orthogonality of Principal Modes of Vibrations, Semi-definitive Systems, Systems with Equal Frequencies, Influence Coefficients, Natural Frequencies and Principal Modes by Matrix Iteration, Damped Free Vibrations, Forced Vibrations

Text Books1. Grover, G. K. (2009) “Mechanical Vibrations” 8th Edition, Nem Chand and Bros

Publisher, ISBN 8185240566, 9788185240565Reference Books

1. Rao, S. S. (2004) “Mechanical Vibrations” 4th Edition, Pearson Education Inc., ISBN 978-81-775-8874-3

2. Kelly, S. G. (2012) “Mechanical Vibrations: Theory and Application, SI” Cengage Learning, ISBN 978-1-4390-6214-2, 1-4390-6214-5

3. Gowda, T., Jagdeesha T. and Girish, D. V. (2012) “Mechanical Vibrations” Tata McGraw Hill Education Private Limited, New Delhi, ISBN 978-1-25-900617-3, 1-25-90U0617-4




Relationship between the Program Outcomes (POs), Program Specific Outcomes (PSOs) and Course Outcomes (COs)PO/CO


CO1 3 1 1 0 0 0 0 0 0 0 0 2 2 1

CO2 3 2 1 0 0 0 0 0 0 0 0 2 2 2

CO3 2 1 - 0 0 0 0 0 0 0 0 2 2 1

CO4 3 1 1 0 0 0 0 0 0 0 0 3 3 2

Average

2.75 1.25 1 0 0 0 0 0 0 0 0 2.25 2.25 1.5


ASEG 3007 Theory of Plates L T P CVersion 1.0 3 0 0 3Pre-requisites/Exposure Mathematics (Integral and Differential calculus)Co-requisites Engineering Mechanics and Strength of Materials

COURSE OBJECTIVES 1. Introduce students to the classical structural mechanics approximations of Membrane, Plate and Shell theories.

2. Use energy formulations to demonstrate the consistent derivation of approximate boundary conditions and edge effects. 3. Demonstrate the analysis tools necessary to describe static, dynamic and non-linear motions. 4. Demonstrate the approximation of the classical formulations using numerical approximation techniques

COURSE OUTCOMESCO1: Understand and appreciate the classical theory of elastic plates.CO2: Analyze the behaviour of plates with uniformly distributed, hydrostatic or concentrated loads.CO3: Apply the structural mechanics approximations of plates and shellsCO4: Determine the static, dynamic, and non-linear motion of membrane, plate and shell structures.

CATALOG DESCRIPTIONThe aim of this module is to introduce the students to the fundamental concepts and principles of the analysis and design of thin-walled shelled structures. The module begins with an introduction to membrane theory for common shapes of axisymmetric structural shells, followed by an overview of buckling. The module introduces the students to the analysis of shells using commercial finite element software including linear elastic, linear plastic, nonlinear elastic and linear buckling analyses.

Course Content UNIT 1: CLASSICAL PLATE THEORY: 6

LECTURE HOURSClassical Plate Theory – Assumptions – Differential Equation – Boundary Conditions.

UNIT 2: PLATES OF VARIOUS SHADES: 12 LECTURE HOURSNavier’s Method of Solution for Simply Supported Rectangular Plates, Leavy’s Method of Solution for Rectangular Plates under Different Boundary Conditions. Governing Equation –Solution for Axi-symmetric loading – Annular Plates – Plates of other shapes.

UNIT 3: EIGEN VALUE ANALYSIS: 4 LECTURE HOURSStability and free Vibration Analysis of Rectangular Plates.

UNIT 4: APPROXIMATE METHODS: 8 LECTURE HOURSRayleigh – Ritz, Galerkin Methods– Finite Difference Method – Application to Rectangular Plates for Static, Free Vibration and Stability Analysis.

UNIT 5: SHELLS: 6 LECTURE HOURSBasic Concepts of Shell Type of Structures – Membrane and Bending Theories for Circular Cylindrical Shells.

Text Books1. Stephen Timoshenko , Theory of Plates & Shells, 2nd edition, Tata McGraw Hill, ISBN-

10: 0070701253, ISBN-13: 978-00707012502. T.H.G. MEGSON, Aircraft Structures for Engineering Students, Fourth Edition,

Butterworth-Heinemann is an imprint of Elsevier, ISBN-13: 978-0-75066-7395, ISBN-10: 0-750-667397

Reference Books1. C.M. Wang and C.Y. Wang, Exact Solutions for Buckling of Structural Members, CRC

Press; 1 edition (27 July 2004), ISBN-10: 0849322227, ISBN-13: 978-08493222282. Stephen Timoshenko, Strength of Materials, CBS; 3 edition (1 December 2002), ISBN-

10: 8123910770, ISBN-13: 978-8123910772.3. D. J. Perry, Aircraft structures, Mc Graw Hill India (2005), ISBN-10: 9339222121,

ISBN-13: 978-9339222123.




Relationship between the Program Outcomes (POs), Program Specific Outcomes (PSOs) and Course Outcomes (COs)PO/CO PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO1

1PO12 PSO1 PSO2


3 2.25 1 1.75 0 0 0 0 0 0 0 0 3 1


ASEG 3008 Supersonic Aerodynamics L T P CVersion 1.0 3 0 0 3Pre-requisites/Exposure Mathematics (Integral and Differential calculus)Co-requisites Engineering Thermodynamics

COURSE OBJECTIVES1. Provide students with a minimum literacy into the origins, purposes, and

methods of gas dynamics.2. To teach students how thermodynamically concepts apply to gas dynamics. 3. To familiarize students with the features of inviscid compressible flows,

including shock waves, expansion fans, and contact surfaces.4. To teach students to analyse or compute one-dimensional and quasi-one-

dimensional flows in typical applications such as supersonic wind tunnels, rocket nozzles, and shock tubes.

COURSE OUTCOMESCO1.Appraise the properties of supersonic and hypersonic flows.CO2. Apply airfoil theory to predict airfoil performance in supersonic flow.CO3. Appreciate the knowledge of basic compressible gas dynamics.CO4: Apply principles of gas dynamics to solve compressible flow problems.CO5: Analyze airfoils at transonic and supersonic flight conditions.CO6: Calculate lift, drag and moment on supersonic airfoils.

CATALOG DESCRIPTIONThis course has a large number of topics dealing with both fundamental and some applied aspects of gas dynamics. It is proposed to expand some of these topics to provide (i) better depth of fundamentals and (ii) inclusion of design related problems. By providing this added depth and related design problems in these areas it is anticipated that the student will receive a much better utilitarian appreciation of gas dynamics. The student is expected to be better prepared for engineering analysis and design which includes elements of gas dynamics.This course studies one-dimensional isentropic flow, nozzles, diffusers, normal and oblique shocks, compressible flow with friction and heating, and an introduction to propulsion systems.

Course Content

UNIT 1: SHOCK WAVES: 11 LECTURE HOURSIntroductory Remarks, Point Source in a Compressible Flow, Mach Waves and Shock Waves.a) Normal Shock waves: equation of motion for a normal shock, normal shock relations for a Perfect Gas, Stagnation Conditions, RH Relations, Propagating Shock Waves, Weak Shock, Reflected Shock Wave, Centered Expansion Waves, Shock Tube. Numerical examples b) Oblique Sock Waves: Introduction, Oblique Shock Relations, M-θ-β Relations, Shock Polar, Supersonic Flow over Wedge, Weak Oblique Shock, Supersonic Compression, Detached Shock. Numerical examples.

UNIT 2: EXPANSION WAVE 7 LECTURE HOURSSupersonic Expansion by Turning, Prandtl-Meyer Flow, Numerical problems. Simple and non simple Regions, Reflection and Intersection of Shocks and Expansion Waves, Mach Reflections, Method of Characteristics, Numerical Examples

UNIT 3: LIFT AND DRAG IN SUPERSONIC FLOWS 6 LECTURE HOURSShock –Expansion Theory, Flow Field in Supersonic, Flow field in Supersonic Flows, numerical problems, Analytical Determination of Lift and Drag Coefficients on Flat Plate, Bi-Convex and Diamond Shaped Sections in Supersonic Flows, numerical problems, Supersonic Leading and Trailing Edges.

UNIT 4: POTENTIAL EQUATION FOR COMPRESSIBLE FLOWS: 4 LECTURE HOURSIntroduction, Crocco’s Theorem, Derivation of Basic Potential Equation For Compressible Flows, Linearization of Governing Equation, Boundary Conditions, Small Perturbation Theory.

UNIT 5: AIRFOILS IN COMPRESSIBLE FLOW 4 LECTURE HOURSIntroduction, Linearized Compressible Flow, Airfoils in Subsonic Flow, Prandtl-Glauert Transformation, Critical Mach Number, Supercritical Flows, Airfoils in Transonic Flow, Governing Equations, Shock Wave Boundary Layer Inter Action.

UNIT 6: MEASUREMENTS IN COMPRESSIBLE FLOWS: 4 LECTURE HOURSRayleigh’s Supersonic Pitot Formula, Equipment used in Supersonic Flows, Supersonic Wind Tunnels, Heat Transfer Tunnels, Shock Tunnels, Aero-Ballistic

Ranges, Terminal Ballistic Range, Rocket Sled Facility, Special Instrumentation for these types of Tunnels.

UNIT 7: HIGH TEMPERATURE GASDYNAMICS: 4 LECTURE HOURSNature of high temperature flows, perfect and real gas, Gibbs free energy and entropy production, microscopic description of gases, thermodynamic properties, equilibirum properties kinetic theory, inviscid high temp. equilibrium and nonequilibrium flow, transport properties.

Text Books1. E. Rathakrishnan, Gas Dynamics, Prentice Hall India Pvt., Limited, 2004, ISBN-

8120309529. 2. John D. Anderson, Fundamentals of Aerodynamics, McGraw

Reference Books1. Balachandran P, Gas Dynamics for Engineers, Prentice Hall India Learning Private

Limited (2010), ISBN: 8120340213.2. H. W. Liepmann and Anatol Roshko, Elements of Gas Dynamics, Dover Publications

Inc. (2002), ISBN-10: 0486419630. 3. Maurice J. Zucrow and Joe D. Hoffman, Gas Dynamics, Wiley India Pvt Ltd; (2013),

ISBN: 81265414314. V. Babu, Fundamentals of Gas Dynamics, Athena Academic Ltd; (2014) ISBN:

1910390003




PO/CO PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 PO12 PSO1 PSO2CO1 3 1 1 0 0 0 0 0 0 0 0 0 3 0CO2 3 3 2 1 0 0 0 0 0 0 0 0 3 1CO3 3 3 2 1 0 0 0 0 0 0 0 0 3 2CO4 3 3 2 2 0 0 0 0 0 0 0 0 3 2CO5 3 3 2 2 0 0 0 0 0 0 0 0 3 2CO6 3 3 2 2 0 0 0 0 0 0 0 0 3 2Average

3 2.67 1.83 1.6 0 0 0 0 0 0 0 0 3 1.8

1= WEEK 2 = MODERATE, 3 = STRONG

SEMESTER VII

ASEG 4001 Flight Mechanics II L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure Basic knowledge of physics and mathematics , Basic

knowledge of Aerodynamics and Flight Mechanics ICo-requisites --

COURSE OBJECTIVES1. To help the students understand the fundamentals and relevance of stability

and control in the broader context of engineering sciences in general, and Aerospace engineering in particular.

2. To enable students to understand theory of flight, apply laws of flight mechanics, and analyse aircraft stability through different aircraft configurations along with the measurement of stability parameters.

3. To empower students with the expertise of experimentation and the fundamental concepts that are required to translate a novel engineering idea to reality through Flight test and Root Locus analysis.

4. To expose students to a wide variety of research areas and concerns in and around flight mechanics such as ILS, UAVs, etc. across multidisciplinary domains.

5. To equip students with necessary engineering skills such as solving engineering problems in a professional way, using commercial software packages such as MATLAB for data analysis, numerical simulations etc.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Apply laws of engineering mechanics to describe aircraft motion. CO2. Estimate stick free longitudinal stability parameters of an aircraft.CO3. Understand and formulate the manoeuvring stability equations CO4. Analyse directional and lateral stability and control characteristics of aircraft.CO5. Apply system vibration concepts on aircraft dynamics.

CATALOG DESCRIPTIONFlight stability and control is an important aspect of aircraft handling qualities for aircraft design and development. The estimation of aircraft neutral point for longitudinal stick fixed and stick free is very important parameter to judge the level of aircraft stability. The directional and lateral stability and control are equally

important aspects of aircraft handling qualities. Finally, knowledge of dynamic stability such as short period motion and phugoid motion, ducth roll motion, etc. also quantify the aircraft handling qualities.The course begins with a detailed analysis of longitudinal stability of airplane due to wing, tail, and engine contributions. The students will learn the fundamental laws of flight mechanics and then flight dynamics of aircraft. The students will thus get an adequate exposure to the techniques used to estimate aircraft handling qualities through theoretical methods as well as flight tests. The student will also learn the art of engineering approximations, and the fundamental concepts of stability and control analysis, that are involved in translating a novel idea to a real-world application. Further, being a rigorous course on problem-solving, it will acquaint students with engineering problem-solving approaches and the effective use of commercial software packages to answer engineering questions.

Course Content UNIT 1: STICK FIXED STATIC LONGITUDINAL STABILITY: 8

LECTURE HOURSIntroduction to Stability of Airplane, Stick Fixed Longitudinal Stability, Effect of Power, Neutral Point, and Center of Gravity Limits. In Flight Measurement of Stick Fixed Neutral Point.

UNIT 2: CONTROL SURFACES AND AERODYNAMIC BALANCING: 4 LECTURE HOURSControl Surface Hinge Moments, Floating and Restoring Tendencies, different types of Tabs used on Airplanes. Frise Aileron, Spoiler Controls.

UNIT 3: STICK FREE STATIC LONGITUDINAL STABILITY: 6 LECTURE HOURSEffect of Free Elevator on Airplane stability, Elevator Control Force, Stick Force Gradients, Neutral Point, Controls Free Center of Gravity Limit. In Flight Measurement of Stick Free Neutral Point.

UNIT 4: MANEUVERING FLIGHT 4 LECTURE HOURSEffect of Acceleration on Airplane Balancing, Elevator Angle per g, and Stick Force per g, Maneuver Margins.

UNIT 5: DIRECTIONAL STABILITY AND CONTROLS: 4 LECTURE HOURS

Asymmetric Flight, Weather Cock Stability, contribution of different parts of Airplane, Rudder Fixed and Rudder Free Static Directional Stability, Rudder Lock.

UNIT 5: LATERAL STABILITY AND CONTROLS: 4 LECTURE HOURSDihedral Effect. Contribution of different. Parts of Airplane Controls in Roll, Aileron Control Power, Cross coupling of Lateral and Directional Effects.

UNIT 6: DYNAMIC STABILITY: 6 LECTURE HOURSSimple Analysis of Short Period and Phugoid Modes, Stick-Fixed and Stick-Free. Lateral and Directional Dynamic Stability: Simple Analysis of Roll Subsdience Spiral Mode and Dutch Roll.

Text Books1. R. C Nelson, Flight Stability and Automatic Control (Second Edition); Mc-Graw Hill2. Bandu N. Pamadi; Performance, Stability Dynamics and Control of Airplanes, AIAA

Education Series 3. Perkins & Hedge; Airplane Performance Stability & Control; John Wiley & Sons

Reference Books

1. Thomus R Yechout, Introduction to Aircraft Flight Mechanics, AIAA Education Series2. McCormick, B. W.; Aerodynamics, Aeronautics, and Flight Mechanics, John Wiley &

Sons, Inc.1995 3. Clancy, L. J. ; Aerodynamics: Sterling Book House, 2006.


Examination Scheme:



PO/CO PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11

PO12 PSO1

PSO2

CO1 2 2 1 2 0 1 0 0 0 0 0 2 3 2

CO2 2 2 1 2 0 1 0 0 0 0 0 2 3 2

CO3 2 2 1 2 0 1 0 0 0 0 0 2 3 2

CO4 2 2 1 2 0 1 0 0 0 0 0 2 3 2

CO5 2 1 1 2 0 1 0 0 0 0 0 2 3 2

Average

2 1.8 1 2 0 1 0 0 0 0 0 2 3 2


ASEG 4002 COMPUTATIONAL FLUID DYNAMICS L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure Strong Knowledge of Fluid Dynamics: Laws governing different

flows, basic equations, flow modeling.Mathematical Expositions: Linear Algebra, Calculus and Probability.

Co-requisites --

COURSE OBJECTIVES1. To present the fundamentals of Computational Fluid Dynamics (CFD) so that

students become knowledgeable users of CFD software.2. To develop a conceptual understanding of numerical methods in terms of the

accuracy, stability, convergence, and other properties of several numerical techniques, amongst the students.

3. To develop an understanding of the applicability and limitations of CFD as a modern design tool amongst students.

4. To introduce the student to widely used techniques in the numerical solution of aerodynamic problems, issues that arise in the solution of such equations, and modern trends in CFD.

5. To enable students with the basic ability to solve and analyze practical fluid mechanics problems drawn from aerospace engineering applications using numerical methods.


1. Understand both flow physics and mathematical properties of governing Navier-Stokes equations and define proper boundary conditions for solution.

2. Demonstrate the systematic application of the mathematical and numerical classification and properties of different state-of-the-art CFD methods as used in engineering practice as well as in research and development

3. Apply knowledge of math and science to engineering by describing continuous fluid-flow phenomena in a discrete numerical sense.

4. Demonstrate a critical awareness of the principles of Computational Fluid Dynamics and concepts of stability, approximation and convergence

5. Demonstrate an understanding of the basic theory behind the approximations used in the finite difference, finite volume, finite element and panel methods in fluid flow problems.

6. Demonstrate a critical awareness of alternative spatial and time discretisation methods for solving fluid mechanics problems governed by the Navier-Stokes/Euler equations

7. Demonstrate a critical awareness of uncertainties and limitations associated with each method.

CATALOG DESCRIPTIONThe Computational Fluid Dynamics (CFD) is a modern tool based numerical solution of equation for fundamental laws for fluid flows. The governing partial differential equations for the conservation of mass, momentum and energy can be solved numerically using high speed digital computers to gain meaning insights into flow behavior as well as heat and mass transfer rates. Besides aerospace engineering, CFD can be used a research and design tool in all fields of engineering involving fluid flow of some kind including flow over spacecrafts to flow inside our arteries. This graduate level course on Computational Fluid Dynamics introduces the numerical computation of continuum fluid flows in engineering applications. The primary focus of the course is on the teaching of numerical methods for the solution of the nonlinear continuum governing fluid equations. Emphasis is placed on finite difference and finite volume numerical formulations. Iterative and temporal solution procedures will also be covered. The students will get hands-on experience with these methods by programming the algorithms and analyzing the physical aspects of the numerical solution. The course provides information that will enable a more sound understanding of black-box commercial software, that are mostly based on finite volume techniques. In addition, it will provide a first step into the large and expanding research area of general computational physics.

Course Content UNIT 1: FUNDAMENTAL CONCEPTS:

10 LECTURE HOURSIntroduction - Basic Equations of Fluid Dynamics, Mathematical Properties of Fluid Dynamics Equations - Elliptic, Parabolic and Hyperbolic Equations - Well Posed Problems - Discretization of Partial Differential Equations -Transformations and Grids - Explicit Finite difference methods of Subsonic, Supersonic and Viscous Flows.

UNIT 2: PANEL METHODS: 03 LECTURE HOURSIntroduction – Source Panel Method – Vortex Panel Method – Applications

UNIT 3: DISCRETIZATION: 08 LECTURE HOURSBoundary Layer Equations and Methods of Solution -Implicit Time Dependent Methods for Inviscid and Viscous Compressible Flows - Concept of Numerical Dissipation -Stability Properties of Explicit and Implicit Methods - Conservative Upwind Discretization for Hyperbolic Systems - Further advantages of Upwind Differencing

UNIT 4: FINITE ELEMENT TECHNIQUES: 07 LECTURE HOURSFinite Element Techniques in Computational Fluid Dynamics; Introduction-Strong and Weak Formulations of a Boundary Value Problem-Strong Formulation-Weighted Residual Formulation - Galerkin Formulation-Weak Formulation-Variational Formulation-Piecewise Defined Shape functions-Implementation of the FEM -The Solution Procedure.

UNIT 5: FINITE VOLUME FORMULATIONS: 08 LECTURE HOURSFinite Volume Techniques - Cell Centered Formulation-Lax Wendoroff Time Stepping- Runge-Kutta Time Stepping-Multi-stage Time Stepping-Accuracy-Cell Vertex Formulation-FDM like Finite Volume Techniques-Central and Upwind Type Discretization- Treatment of Derivatives.

Text Books1. John D Anderson, Jr., Computational Fluid Dynamics -The Basics with Applications,

McGraw Hill, 1995.2. H. K. Versteeg and W. Malalasekera, An Introduction to Computational Fluid Dynamics

- The Finite Volume Method, Longman Scientific and Technical, 1995.

Reference Books1. Tapan K. Sengupta, Theoretical and Computational Aerodynamics, John Wiley & Sons

Ltd., 2015.2. Joel H. Ferziger and Milovan Peric, Computational Method for Fluid Dynamics, 3rd

Edition, Springer, 2002.3. Dale A. Anderson, John C. Tannehill and Richard H. Pletcher, Computational Fluid

Mechanics and Heat Transfer, 2nd Edition, Taylor and Francis, 1984.


Components Internal MSE ESE

AssessmentWeightage (%) 30 20 50


PO/CO PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 P012 PSO1 PSO2CO1 3 1 0 0 1 0 0 0 0 0 0 0 3 2CO2 3 1 0 0 2 0 0 0 0 0 0 0 3 2

CO3 3 0 0 1 3 0 0 0 1 0 0 2 3 2CO4 2 0 0 1 3 0 0 0 1 0 0 2 3 2CO5 2 0 0 1 3 0 0 0 1 0 0 2 3 2CO6 3 0 0 1 3 0 0 0 1 0 0 2 3 2Avg. 2.7 1 0 1 2.5 0 0 0 1 0 0 2 3 2


ASEG 4003 FINITE ELEMENT METHODS L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure Conceptual knowledge in systems of structural and fluid analysis.

Strong mathematical grasp of Varitional formulation of functions and governing equations of general systems

Co-requisites --

COURSE OBJECTIVES1. To provide the fundamental concepts of the theory of the finite element

method.2. To develop proficiency in the application of the finite element method

(modeling, analysis, and interpretation of results) to realistic engineering problems through the use of a major commercial general-purpose finite element code.

3. To introduce basic aspects of finite element technology, including domain discretization, polynomial interpolation, application of boundary conditions, assembly of global arrays, and solution of the resulting algebraic systems

COURSE OUTCOMES On completion of this course, the students will be able toCO1: Understand the basics of finite element methods and element propertiesCO2: Understand the properties of isoparametric element and one-dimensional element.CO3.Apply the knowledge of FEA in solving the plane stress, plane strain, plane bending and conduction heat transfer problem.CO4: Interpret direct stiffness method and solution techniques.CO5: Apply the knowledge of finite elements methods to solve problem in aerospace domain using finite element analysis software.

CATALOG DESCRIPTIONThe finite element method is an indispensable tool for engineers in all disciplines. This course introduces students to the fundamental theory of the finite element method as a general tool for numerically solving differential equations for a wide range of engineering problems. Field problems described by the Laplace, and Poisson equations are presented first and all steps of the FE formulation are

described. Specific applications in heat transfer and flow in porous media are demonstrated with associated tutorials. The application of the method to elasticity problems is then developed from fundamental principles. Specific classes of problems are then discussed based on abstractions and idealizations of 3D solids, such as plane stress and strain, Euler-Bernoulli and Timoshenko beams and Kirchoff and Mindlin-Reissner plates and shells. Time dependent problems and time integration schemes are presented. Special topics such as multiple constraints, mixed formulations and sub structuring are introduced. Finite element formulation for incompressible flow problems is introduced through discretization of Euler and Navier-Stokes equations.

Course Content UNIT 1: INTRODUCTION: 4 LECTURE

HOURSField conditions, boundary conditions, functional approximation, finite differences method, development of finite element method.

UNIT 2: ELEMENT PROPERTIES: 4 LECTURE HOURSDisplacement models, relation between the nodal degrees of freedom and generalized coordinates, convergence requirements, natural co-ordinate systems, shape functions, element strains and stresses, development of element stiffness, matrix and equivalent nodal loads, static condensation.

UNIT 3: ISOPARAMETRIC ELEMENTS: 4 LECTURE HOURSIsoparametric, super-parametric and sub-parametric elements, computation of stiffness matrix of isoparametric elements, convergence criteria for isoparametric elements, numerical integration technique using Gauss Quadrature.

UNIT 4: ONE DIMENSIONAL ELEMENT: 4 LECTURE HOURSTruss element, analysis of plane truss problem, Hermitian beam element, beam on elastic foundation, solution of beam problem.

UNIT 5: PLANE STRESS AND PLANE STRAIN ANALYSIS: 4 LECTURE HOURSTriangular elements, rectangular elements, isoparametric elements, patch test, axisymmetric solid element.

UNIT 6: PLANE BENDING ANALYSIS: 4 LECTURE HOURSDisplacement functions, plate bending elements, reduced integration, stress smoothing technique.

UNIT 7: CONDUCTION HEAT TRANSFER: 4 LECTURE HOURSFormulation of finite element method for heat conduction, various weighted residual techniques, one dimensional heat conduction, two dimensional conduction heat transfer.

UNIT 8: DIRECT STIFFNESS METHOD OF ANALYSIS AND SOLUTION TECHNIQUE: 4 LECTURE HOURSAssemblage of elements, direct stiffness method, boundary conditions and reactions, Gauss elimination and matrix decomposition.

UNIT 9: FINITE ELEMENT ANALYSIS SOFTWARE: 4 LECTURE HOURSPre-and Post-processors finite element analysis software, error estimates and adaptive meshing.

Text Books1. An Introduction to the Finite Element Method, J. N. Reddy; McGraw Hill Education.

Reference Books

1. Textbook of Finite Element Analysis; P. Seshu; PHI Learning Private LTD. 2. The Finite Element Method-Its Basis & Fundamentals, O. C. Zienkiewicz, R. L. Taylor

& J. Z. Zhu; Butterworth-Heinemann

3. Finite Element Method with Applications in Engineering; Y.M. Desai, T. I. Eldho & A. H. Shah, Pearson


Examination Scheme:



PO/CO PO1

PO2 PO3

PO4

PO5 PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

CO1 1 0 0 0 0 0 0 0 0 0 0 0 0 0

CO2 1 0 0 0 0 0 0 0 0 0 0 0 1 0

CO3 3 2 0 0 1 0 0 0 0 0 0 0 1 0

CO4 3 2 1 0 1 0 0 0 0 0 0 0 2 0

CO5 3 3 2 3 3 0 0 0 0 0 0 2 1 2

Average

2.2 2.33 1.5 3 1.66

0 0 0 0 0 0 2 1.25 2


ASEG 4006 Orbital Mechanics L T P CVersion 1.0 3 0 0 3Pre-requisites/Exposure Dynamics, Linear Algebra and Differential EquationsCo-requisites --

COURSE OBJECTIVES1. Develop an understanding of orbital mechanics. 2. Obtain a detailed knowledge of the two-body problem and its solutions with

applications to geocentric orbits and interplanetary transfers. 3. Understand the concept of impulsive thrusting and its use in orbital transfers

including plane changes.4. Obtain a knowledge of Kepler’s laws, eccentricity and true anomaly5. Understand and be able to apply Lambert’s theorem for the time-of-flight on

the parabola and hyperbolic

COURSE OUTCOMES On completion of this course, the students will be able toCO1. An ability to find characteristics of desired transfer trajectories and the corresponding specific impulses.CO2. An ability to solve problems requiring the design of interplanetary trajectories.CO3. An ability to use MatLab for the numerical solution of Lambert’s problem and Gauss problem

CATALOG DESCRIPTIONThis course covers the fundamentals of astrodynamics, focusing on the two-body orbital initial-value and boundary-value problems with applications to space vehicle navigation and guidance for lunar and planetary missions, including both powered flight and midcourse maneuvers. Other topics include celestial mechanics, Kepler's problem, and Lambert’s problem.

Course Content UNIT 1: ASTRODYNAMICS: 22

LECTURE HOURSGeneral Laws of Mechanics, inertial frames of reference, work energy, angular momentum. Two-Body Problem and central force motion, orbits as conic section, elliptical orbits.

Kepler’s laws, determination of the eccentricity and the true anomaly, Single impulse adjustment.

UNIT 2: MECHANICS: 14 LECTURE HOURSHohmann transfer, other coplanar transfer, change of plane, hyperbolic and parabolic orbits, Lamberts theorem, Three – Body Problem.

Text Books

1. Howard C. Curtis, Orbital Mechanics for Engineering Students, Elsevier, 2005

Reference Books1. Battin, Richard. An Introduction to the Mathematics and Methods of Astrodynamics.

Revised ed. Reston, VA: AIAA, 1999. ISBN: 9781563473425




CO/PO PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

CO1 2 2 1 2 2 0 1 0 0 1 0 1 2 0

CO2 1 2 1 2 2 0 1 0 0 1 0 1 1 1

CO3 2 2 1 2 2 0 1 0 0 1 0 2 1 0

Average

1.67

2 1 2 2 0 1 0 0 1 0 1.33 1.33 1


ASEG 4007 Helicopter Engineering L T P CVersion 1.0 3 0 0 3Pre-requisites/Exposure Basic knowledge of aerodynamics and Flight MechanicsCo-requisites

COURSE OBJECTIVES1. To help the students understand the fundamentals and relevance of Rotary

wing Aerodynamics for Helicopter motion.2. To enable students to apply laws of fight theory, and analyse Helicopter

performance in different flight regimes.3. To empower students with the expertise of Helicopter stability analysis. 4. To expose students to different components of Helicopter such as Rotor,

fuselage in context to vibrations.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Understand fundamentals of Helicopter rotor blade motion.CO2. Calculate Helicopter Rotor performance parameters.CO3. Understand Helicopter trim and performance.CO4. Estimate dynamic stability of Helicopter.CO5. Decode the sources of Helicopter vibrations.

CATALOG DESCRIPTIONHelicopters have wide variety of applications in civil as well as defense sectors. The Indian manufacturing industry is eyeing on Helicopter manufacturing in the country. Hence, this course is important in order to prepare professionals with required level of understanding and analysis skills in Helicopter engineering. This course is

transition from fixed wing to rotary wing through extending regular theories of aerospace engineering to Helicopter Engineering applications. Historical developments are very important aspect to inculcate the level of interest in Helicopter Engineering. The course begins with a historical perspective of Helicopter developments that took place in aviation. The students then learn about working principle of Helicopter rotor mechanism. The students will thus get an adequate exposure to the techniques used to estimate helicopter basic aerodynamics through theoretical methods. The student will also learn the art of engineering approximations, and the fundamental concepts of Helicopter engineering, that are involved in translating a novel idea to a real-world application. Further, it will acquaint students with knowledge of working principle of Helicopter components to answer aerospace engineering questions.

Course Content UNIT 1: INTRODUCTION: 8 LECTURE

HOURSHistorical development, configuration of helicopter, rotor systems and flight control mechanism

UNIT 2: HELICOPTER PERFORMANCE: 16 LECTURE HOURSMomentum theory and blade element theory in hover, vertical flight and forward flight. Idealization of rotor blade, flap- lag and torsional dynamics of blade

UNIT 3: HELICOPTER CONTROL 12 LECTURE HOURSTrim and equilibrium analysis, flap-pitch, lag- pitch and flap-lag coupling, simple model of rotor fuselage dynamics, longitudinal and lateral stability and control of helicopters.

Text Books1. J, Seddon, Basic Helicopter Aerodynamics, BSP Professional Books, 19902. Bramwell, A.R.S, Helicopter Dynamics, Butterworth Heinemann, 1976

Reference Books1. Johnson, Wayne; Rotorcraft Aeromechanics, 20132. Jacob Shapiro: Principles of Helicopter Engineering




PO/CO PO1 PO- PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 PO12 PSO1 PSO2CO1 2 1 1 1 0 1 0 0 0 0 0 1 3 1

CO2 2 2 2 2 0 1 0 0 0 0 0 1 3 2

CO3 2 2 2 2 0 1 0 0 0 0 0 1 3 2

CO4 2 2 2 2 0 1 0 0 0 0 0 1 3 2

CO5 2 1 2 1 0 1 0 0 0 0 0 1 3 1

Avg. 2 1.6 1.8 1.6 0 1 0 0 0 0 0 1 3 1.6


SEMESTER:- VIII

ASEG 4004 Aircraft Design L T P CVersion 1.0 3 1 0 4Pre-requisites/Exposure Knowledge of Aerodynamics , Propulsion, Flight Mechanics

Co-requisites --

COURSE OBJECTIVES1. Familiarize students with the important issues and methodologies of aircraft

design. 2. Illustrate the process of aircraft synthesis as an outcome of the integration of

the disciplines of aerodynamics, performance, stability and control, propulsion, structures and aeroelasticity.

3. Introduce students to CAD drawing and rapid prototyping to make a small 3-D model of the final design.

4. Develop the ability to function as a member of a team in a design setting; including the ability to conduct a peer review of the other team members.

5. Familiarize students with Federal Aviation Regulations as a means for ensuring passenger safety.

6. Further enhance and develop technical communication skills.

COURSE OUTCOMES On completion of this course, the students will be able toCO1.Appraise preliminary design process of a complete aircraft based on the specifications provided.CO2. Conduct trade-off between the conflicting demands of different disciplines by performing a detailed preliminary design of a complete aircraft. CO3.Assess various aircraft parameters and their effect of performanceCO4.Design a system, component, or process that meets given requirements in aircrafts.CO5. Demonstrate familiarity with aircraft safety based on FAA regulationsCO6. Work effectively as a member of a multidisciplinary design team.

CATALOG DESCRIPTIONMultidisciplinary integration of aerodynamics, performance, stability and control, propulsion, structures and aeroelasticity in a system approach aimed at designing an aircraft for a set of specifications. Includes weight estimates, configuration and

powerplant selection, tail-sizing, maneuver and gust diagrams, wing loading, structural and aeroelastic analysis. Students work in teams, effective teamwork nurtured.

Course Content UNIT 1: PRELIMINARIES: 7 LECTURE

HOURSAircraft Design, Requirements and Specifications, Airworthiness Requirements. Weight: It's Importance. Aerodynamic and Structural Design Considerations. Classifications of Airplane, Concept of Configuration Design special features.

UNIT 2: AIR LOADS IN FLIGHT: 9 LECTURE HOURSSymmetrical Maneuvering Loads in Flight, Load Factor V-N Diagram, Gust Loads, Estimation of Gust Loads, Structural Effects.

UNIT 3: WING DESIGN CONSIDERATIONS: 7 LECTURE HOURSSelection of Airfoil and Plan Form. Span Wise Air Loads Variation, BM and SF. Design Principles for the Structure of all Metal, Stressed Skin Wing (Civil & Military Airplane).

UNIT 4: CONCEPTUAL DESIGN OF AIRPLANE AND LAYOUT: 9 LECTURE HOURSPreliminary Aerodynamic Design of an Airplane for a given set of specification (Civil / Military). Preparation of 3-views and layout. Estimation of Performance: Take-Off, Landing, Climbing Cruise, Flight Envelope.

UNIT 5: LAUNCH VEHICLE DESIGN: 4 LECTURE HOURSFundamentals of Launch Vehicle Design, Stability and Control, and Handling qualities, Spacecraft Layout.

Text Books1. Anderson, John D. “Aircraft performance and Design” Tata McGraw Hill Publishing

Company, New Delhi

Reference Books1. Daniel P. Raymer, G. “Aircraft Design A Conceptual Approach” American Institute of

Aeronautics and Astronautics, Inc., Washington, DC2. Jan Roskam “Airplane Design Part I-VIII”, DAR Corporation, 2000 3. John P Fielding – “Introduction to Aircraft Design”, Cambridge University Press, 2005




PO/CO PO1

PO-

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

CO1 1 1 3 1 1 1 1 0 0 0 0 1 3 3

CO2 1 2 1 1 1 1 1 0 0 0 0 1 3 3

CO3 3 2 3 2 2 1 1 0 0 0 0 1 3 3

CO4 3 2 3 2 2 1 1 0 0 0 2 3 3 3

CO5 2 2 3 1 2 1 1 0 0 0 2 2 3 3

Averagre

2 1.8 2.6 1.4 1.6 1 1 0 0 0 2 1.6 3 3


ASEG 4008 Space Science & Space Environment L T P CVersion 1.0 3 0 0 3Pre-requisites/Exposure Vector Calculus, Relativistic PhysicsCo-requisites --

COURSE OBJECTIVES1. Understand the Environment in details 2. Able to understand the properties of the atmosphere and near Space

Environment including Van Allen Belts3. Be able to understand the near Earth system and especially Earth-Moon

System4. Understanding of the solar system and the planets. Analysis of Oort Cloud,

Asteroids, Comets, Heliopause5. Understanding of the Sun, the Layers of the Sun, Sun Spots, Solar Wind, solar

Ejections, Fusion Process in the Sun, Harmonics of the Sun6. Understanding the concept of space weather and its effects on the near Earth

environment, effects on satellites and aviation, effect of space weather on ground power systems, communication- GPS systems, effect on oil pipes

7. Cosmic Rays, Interstellar Space, Nearby Clusters and Galaxies8. Understanding of Basic Astronomy, Absolute-Apparent Brightness, Parsec,

Measurements, Relation Between Temperature-Mass-Brightness of Objects9. Basics of Cosmology, Evolution of Stars, Big Bang Theory, Big Crunch Theory,

Effects of Blackholes on Mechanics of Space

COURSE OUTCOMES On completion of this course, the students will be able toCO1.Understand the1 astronomy, measurements, Solar systems.CO2.Evaluate the properties of the Earth’s Atmosphere and its properties.CO3.Demonstrate and understanding of the theory behind motion of van Allen particles.CO4.Appraise the space weather and their effects on earth environment.

CATALOG DESCRIPTIONThis is an introductory course includes topics such as Introduction to selected topics in astronomy, with emphasis on the conditions in the Sun and solar system: interplanetary space, solar-terrestrial and Earth-Moon systems. Properties of the

upper atmosphere, ionosphere, magnetic field, and magnetosphere of the Earth. Theory of motion of charged particles in electric and magnetic fields with application to Van Allen particles and cosmic rays. The solar wind and its interaction with the Earth, Introduction to Cosmology and Big Bang Theory, Evolution of stars

Course Content UNIT 1: INTRODUCTION:

14 LECTURE HOURSIntroduction to selected topics in astronomy, with emphasis on the conditions in the Sun and solar system: interplanetary space, solar-terrestrial and Earth-Moon systems.

UNIT 2: PROPERTIES OF ATMOSPHERE: 8 LECTURE HOURSProperties of the upper atmosphere, ionosphere, magnetic field, and magnetosphere of the Earth.

UNIT 3: THEORY OF MOTION: 8 LECTURE HOURSTheory of motion of charged particles in electric and magnetic fields with application to Van Allen particles and cosmic rays.

UNIT 4: SOLAR WIND: 6 LECTURE HOURSThe solar wind and its interaction with the Earth.

Text Books1. Space Science, by Louise K. Harra (Imperial College Press)

Reference Books1. Introduction to Space Science, by W. Hess2. Introduction to Space Physics, by Kivelson and Russell




CO/PO PO1

PO2

PO3

PO4

PO5

PO6

PO7

PO8

PO9

PO10

PO11

PO12

PSO1

PSO2

CO1 1 2 0 3 2 1 2 0 0 2 0 1 2 0

CO2 1 1 0 2 2 1 2 0 0 2 0 1 1 0

CO3 1 1 0 2 2 0 2 0 0 2 0 1 1 0

CO4 1 2 0 2 3 1 3 0 0 2 0 2 2 0

Average

1 1.5 0 1.75

1.75

1 1.75

0 0 2 0 1.25 1.5 0


ASEG 4009 Composite Materials L T P CVersion 1.0 3 0 0 0Pre-requisites/Exposure Basic knowledge of material science especially on the metals,

ceramics and polymers.Co-requisites --

COURSE OBJECTIVESThe objectives of this course are to:

1. Introduce students the concepts of modern composite materials, and their constituents i.e. fibres and matrix.

2. Enable students with knowledge on how to fabricate and carry out standard mechanical test on composites to determine mechanical properties for aerospace applications.

COURSE OUTCOMES On completion of this course, the students will be able toCO1.Identify and explain the types of composite materials, their structures and properties. CO2.Understand and explain the fabrication methods employed for composite preparation.

CO3.Illustrate the factors that influence the performance and degradation of composite materials for aerospace applications.CO4.Select composite materials for desired applications i.e. aerospace, automobile and energy.CO5.Identify the research and new developments of advanced composite materials for aerospace Applications.

CATALOG DESCRIPTIONThe composite materials are widely applicable in fabrication of various objects like aircraft, automobile parts and energy related devices. In this course, the students will be given the basics idea about the composite materials and the reasons for the need of composite materials. They will learn about the classifications of composite materials according to the nature of the matrix (Polymer, Metal, Ceramics) and the reinforcement (fibers, whiskers, particulates). The students will develop the idea about the variation of specific strength and stiffness of high-performance composite materials as well as their failure criteria. Further the students will learn about fabrication processes for composite materials with high mechanical properties. At the end, the students will be able to choose the correct composite materials and also they will be able to carry out independent research on advanced composite materials for desired applications

Course Content UNIT 1: INTRODUCTION TO COMPOSITES 6

LECTURE HOURSFundamentals of composites - need for composites – Enhancement of properties-classification of composites – Matrix-Polymer matrix composites (PMC), Metal matrix composites (MMC), Ceramic matrix composites(CMC)–Reinforcement–Particle reinforced composites, Fibre reinforced composites. Applications of various types of composites.

UNIT 2: POLYMER MATRIX COMPOSITES 8 LECTURE HOURSPolymer matrix resins – Thermosetting resins, thermoplastic resins – Reinforcement fibres – Rovings – Woven fabrics – various types of fibres. PMC processes - Hand lay-up processes – Spray up processes – Compression moulding – Reinforced reaction

injection moulding - Resin transfer moulding – Pultrusion – Filament winding – Injection moulding. Fibre reinforced plastics (FRP), Glass fibre reinforced plastics (GRP).

UNIT 3: METAL MATRIX COMPOSITES 8 LECTURE HOURS Characteristics of MMC, Various types of Metal matrix composites Alloy vs. MMC, Advantages of MMC, Limitations of MMC, Metal Matrix, Reinforcements – particles – fibres. Effect of reinforcement - Volume fraction – Rule of mixtures. Processing of MMC – Powder metallurgy process - diffusion bonding – stir casting – squeeze casting.

UNIT 4: CERAMIC MATRIX COMPOSITES 8 LECTURE HOURS Engineering ceramic materials – properties – advantages – limitations – Monolithic ceramics - Need for CMC – Ceramic matrix - Various types of Ceramic Matrix composites- oxide ceramics – non oxide ceramics – aluminium oxide – silicon nitride – reinforcements – particles- fibres- whiskers. Sintering - Hot pressing – Cold isostatic pressing (CIPing) – Hot isostatic pressing (HIPing).

UNIT 5: ADVANCES IN COMPOSITES 6 LECTURE HOURS Carbon / carbon composites – Advantages of carbon matrix – limitations of carbon matrix Carbon fibre – chemical vapour deposition of carbon on carbon fibre perform. Sol gel technique. Composites for aerospace applications.

Text Books1. D. Hull, T. W. Clyne, Introduction to composite materials (1996). Cambridge University

Press. ISBN 978-05213885592. Robert Jones, Mechanics of composite materials (1998), CRC Press, Taylor & Francis.

ISBN: 1-56032-712-X3. P. K. Mallick, Fiber Reinforced Composite (2007), CRC Press, Taylor & Francis. ISBN:

13: 978-0-8493-4205-9

Reference Books1. L.J. Broutman and R.M.Krock (1997) “Modern Composite Materials” Addison-Wesley

Educational Publishers Inc. ISBN: 978-0201006292 2. K.K.Chawla “Composite Materials – Science and Engineering (2016)” ISBN: 978-

1493950157

Modes of Evaluation: Quiz/Assignment/ Common Class Tests/ Tutorial classes/ Written ExaminationExamination Scheme:



PO/CO PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 PO12 PSO1 PSO2CO1 3 2 0 0 0 0 0 0 0 0 0 0 3 0

CO2 2 2 2 0 0 0 0 0 0 0 0 0 2 1

CO3 2 2 2 0 0 0 0 0 0 0 0 0 2 1

CO4 2 2 2 0 0 0 0 0 0 0 0 0 2 1

CO5 2 2 2 0 0 0 0 0 0 0 0 0 2 1

Average

2.2 2 2 0 0 0 0 0 0 0 0 0 2.2 1


ASEG 4010 Aero-Elasticity L T P CVersion 1.0 3 0 0 3Pre-requisites/Exposure Mathematics (Integral and Differential calculus)Co-requisites Elements of vibration Aerodynamics and Flight Mechanics

COURSE OBJECTIVESAn introduction to linear aeroelasticity, covering aerodynamic and dynamic structural phenomena associated with flexible airplanes and missiles. Topics include divergence of linear elastic lifting surfaces; vibration of discrete and continuous systems; effect of elastic deformations on lift distributions and stability; flutter of linear elastic straight and swept wings employing both discrete and distributed models; introduction to stochastic processes; Dynamic response to gust loads and continuous atmospheric turbulence.

COURSE OUTCOMESCO1: Formulate and solve classical aeroelastic problems.CO2: Appreciate the significance of load redistribution in the response of aerospace vehicles.CO3: Understand the static and the dynamic aeroelastic instabilities such as divergence, control surface reversal and flutter.CO4: Realize the effect of unsteady aerodynamics on the behavior of aeroelastic systems, CO5: Incorporate the aeroelastic constraints into the design aerospace structure.

CATALOG DESCRIPTIONAeroelasticity is the interaction between structural dynamics and unsteady aerodynamic flow over the structure. It is an important area of study for two main reasons. First the interaction can lead to static or dynamic instabilities which can result in failure of the structure. Secondly the loads calculated using aeroelastic simulations are significantly different for flexible structures compared to decoupled structural and aerodynamic simulations. This has a significant influence on the design and weight of the structure, and its aerodynamic performance. Therefore it is important to take aeroelastic effects into account in the design of structures. This course will be of value to professionals working in the design and production of aircraft and helicopter components, wind turbine and other aerodynamic structures.

For students of aerodynamics this course will advance their knowledge and understanding of aeroelastic phenomena and their effect.

Course Content

UNIT 1: INTRODUCTION: 8 LECTURE HOURS Definition and Historical Background, Static and Dynamic Aeroelastic Phenomenon, Integration of Aerodynamic, Elastic and Inertia Forces, Influence of Aeroelstic Phenomenon on Air Craft Design, Comparison of Critical Speeds.

UNIT 2: DIVERGENCE OF LIFTING SURFACE: 12 LECTURE HOURSThe Phenomenon of Divergence, Divergence of 2-D Wing Section, Divergence of an Idealized Cantilever Wing, Solution based on Semi-Rigid Assumptions, Solution to Generalized Co-Ordinates Method of Successive Approximation, use of Numerical Methods.

UNIT 3: STEADY STATE AERO-ELASTICITY PROBLEMS IN GENERAL:8 LECTURE HOURS

Loss and Reversal of Aileron Control: 2D Case, Aileron Reversal General Case. Lift Distribution on a Rigid and Elastic Wing. Effect on Static Longitudinal Stability of Airplane.

UNIT 4: INTRODUCTION TO FLUTTER AND BUFFETING: 8 LECTURE HOURSThe Phenomenon of Flutter, Flutter of a Cantilever Wing. Approximate Determination of Critical Speed by Galerkin’s Method, Buffeting and Stall Flutter--an introduction.

Text Books1. Y C Fung, An Introduction to the Theory of Aero-elasticity, Dover Publications, INC,

Mineola, New York, ISBN-0-486-49505-1.2. T.H.G. MEGSON, (2-12) Aircraft Structures for Engineering Students, Fourth Edition,

Butterworth-Heinemann is an imprint of Elsevier, ISBN-13: 978-0-75066-7395, ISBN-10: 0-750-667397

Reference Books1. Jan R. Wright, Jonathan Edward Cooper, Introduction to Aircraft Aero-elasticity and

Loads, 2nd Edition, Wiley Publication, ISBN: 978-1-118-48801-0 2. Raymond L. Bisplinghoff, Holt Ashley, Robert L. Halfman, Aeroelasticity, Courier

Corporation, 1996, ISBN 0486691896, 9780486691893.3. Balakrishnan, AV, Aeroelasticity: The Continuum Theory, Springer-Verlag New York,

eBook ISBN 978-1-4614-3609-6, Hardcover ISBN 978-1-4614-3608-9.

4. Rama B. Bhat, Principles of Aeroelasticity, CRC Press, ISBN 9781498724722 - CAT# K25741




PO/CO PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 PO12 PSO1 PSO2CO1 3 2 2 2 0 0 0 0 0 0 0 0 3 0CO2 3 3 2 3 0 0 0 0 0 0 0 0 3 1CO3 3 3 3 3 0 0 0 0 0 0 0 0 3 2CO4 3 3 2 3 0 0 0 0 0 0 0 0 3 2CO5 3 3 2 3 0 0 0 0 0 0 0 0 3 2Average

3 2.8 2.2 2.8 0 0 0 0 0 0 0 0 3 1.75


ASEG-4011 Rocket Propulsion L T P CVersion 1.0 3 0 0 3Pre-requisites/Exposure Basic knowledge of Aerospace propulsion system

and knowledge of basic thermodynamics and combustion

Co-requisites Orbital Mechanics

COURSE OBJECTIVES1. To help the students to understand the motion in space and definition of

space in context of space aircraft.2. To empower students to differentiate the types of propulsive devices used in

space and impact of the historical development of rocket engine in current generation.

3. To expose students to analyse the flow physics of combustion inside the thrust chamber and predict the actual performance of the engine by applying all basics principles of engineering.

4. To equip students with necessary engineering skills such as solving engineering problems in a space domain and do an actual case analysis of rocket engine to enhance the technical skill, team work and presentation skill in order to meet the industry requirement.

COURSE OUTCOMES On completion of this course, the students will be able toCO1. Understand the motion in space and types of propulsive devices used in space.CO2. Examine the flow physics of combustion inside the thrust chamber. CO3. Calculate space vehicle performance (aerothermal analysis) parameters and its stages.CO4. Estimate Propellants combustion properties for given rocket engine specification.CO5. Select the space vehicles and advance energy source rocket for given mission.

CATALOG DESCRIPTIONPropulsion is very important for any kind of engine and one of the leading application is aerospace. It includes all the thrust mechanism and all basic components of the engine. Rocket propulsion is very specific application from aerospace domain, under which study of motion of space and definition of space will

be taught. Through the knowledge of rocket propulsion one can able to estimate the requirement of size of thrust chamber, nozzle and how much mass is needed for particular mission.Rocket science deals about all the aspect of the rocket in space but propulsion taught how to move vehicle in space and all relative theory. This course is restricted to propulsion only where historical development of rocket will be the key to design a new challenge in space era. The course begins to space definition and development of rocket with different types of rocket. Further unit will give knowledge to student to estimate the all performance of rocket like thrust, specific impulse, specific propellants consumptions etc. The student will also learn the all fundamental law and principal used in space vehicles. By applying all the law and basic principal student can estimate all the parameters of rocket engine and analyze the flow inside the thrust chamber as well as in nozzle. Further unit emphasizes the nozzle theory which deals about all the parameters like stagnation pressure, stagnation temperature etc. will effect on nozzle performance. At the end of the unit student can able to understand how to select the rocket engine for the particular mission, and also argue on selection of propellants used in the particular application like solid propellant used for low altitude whereas liquid and hybrid can be used for long range.

Course Content UNIT 1: INTRODUCTION 10 LECTURE

HOURSTypes of propulsion systems, thrust, equivalent exhaust velocity, specific impulse and mass ratio, single stage and multistage rockets, Nozzle thrust coefficient mission analysis, orbit overview.

UNIT 2: ROCKET PERFORMANCE 14 LECTURE HOURSIdeal thermodynamics of liquid rocket engines calculation of rocket thrust via momentum equation Ideal expansion, over/Under Expansion Chemical Rockets, Rocket Nozzle Performance

UNIT 3: CLASSIFICATION OF ROCKETS 12 LECTURE HOURS Aero-thermochemistry of liquid and solid propellant Rockets, Exhaust velocity analysis with Frozen and Equilibrium flow consideration, Nonchemical Rockets,

nuclear Heated rockets, Electrically Powered Rockets, Lorentz Accelerator in a constant area duct.

Text Books1. George P. Sutton, Rocket Propulsion Elements (Seventh Edition) 2. K. Ramamurthi, Rocket Propulsion, Macmillan, in 2010

Reference Books

1. Hill, P. G. and Peterson, C.R., Mechanics and thermodynamics of propulsion, 2nd ed., Reading, Massachusetts: Addison Wesley Publishing Company,, 1992.

2. H S Mukunda, Understanding Propulsion, Interline Bangalore in 2004




PO/CO


CO1 3 1 0 0 0 0 0 0 0 0 0 0 3 2CO2 2 2 0 0 0 0 0 0 0 0 0 0 2 2CO3 2 2 3 3 2 0 1 0 2 0 0 2 3 3CO4 3 2 2 0 0 0 0 0 0 0 0 0 3 2C05 3 2 1 2 0 0 1 0 0 0 0 2 3 2Average

2.6 1.8 2 2.52 2 0 1 0 2 0 0 2 2.8 2.2


Documents

Text Books - upes.ac.in · Web viewOrigin of X-rays, Continuous X-ray Spectra, Production of Characteristic X-Ray spectra, Moseley’s law, ... Mahajan S. (2009) Modern Physics,