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THE GATE ACADEMY's GATE Correspondence Materials consist of complete GATE syllabus in the form of booklets with theory, solved examples, model tests, formulae and questions in various levels of difficulty in all the topics of the syllabus. The material is designed in such a way that it has proven to be an ideal material in-terms of an accurate and efficient preparation for GATE. Quick Refresher Guide : is especially developed for the students, for their quick revision of concepts preparing for GATE examination. Also get 1 All India Mock Tests with results including Rank,Percentile,detailed performance analysis and with video solutions GATE QUESTION BANK : is a topic-wise and subject wise collection of previous year GATE questions ( 2001 – 2013). Also get 1 All India Mock Tests with results including Rank,Percentile,detailed performance analysis and with video solutions Bangalore Head Office: THE GATE ACADEMY Jayanagar 4th block E-Mail: [email protected] Landline: 080-61766222
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Strength of Materials
For
Mechanical Engineering
By
www.thegateacademy.com
Syllabus SOM
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Syllabus for
Strength of Materials
Stress and strain, stress-strain relationship and elastic constants, Mohr’s circle for plane stress and plane
strain, shear force and bending moment diagrams, bending and shear stresses, deflection of beams,
torsion of circular shafts, thin and thick cylinders, Euler’s theory of columns, strain energy methods,
thermal stresses.
Analysis of GATE Papers
(Strength of Materials)
Year Percentage of marks Overall Percentage
2013 5.00
8.29%
2012 11.00
2011 9.00
2010 5.00
2009 6.00
2008 13.33
2007 8.00
2006 8.00
2005 9.33
Content SOM
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C O N T E N T S
Chapters Page no.
#1. Simple Stress and Strain 1 – 33
Introduction 1
Simple Stress & Strain 1
Hooke’s Law 1 – 2
Stress – Strain Diagram 3 – 4
Possion’s Ratio 4 – 5
Cylindrical Pressure Vehicle 5 – 6
Spherical Pressure Vehicle 7
Solved Examples 8 – 21
Assignment – 1 22 – 24
Assignment – 2 24 – 27
Answer keys 28
Explanations 28 – 33
#2. Shear Force and Bending Moment 34 - 58
Introduction 34
Shear and Moment 34 – 35
Shear Force and Bending Moment Relationships 35 – 37
Propped Means & Fixed Beams 37 – 40
Singularity Function 40 – 41
Solved Examples 42 – 48
Assignment – 1 49 – 52
Assignment – 2 52 – 54
Answer keys 55
Explanations 55 – 58
#3. Stresses in Beams 59- 76
Introduction 59
Bending Stress 59 – 60
Important Points 60
Shear Stress 61 – 62
Composite Beams 62
Solved Examples 63 – 67
Assignment – 1 68 –70
Assignment – 2 70 – 71
Content SOM
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Answer keys 72
Explanations 72 – 76
#4. Deflection of Beams 77 - 105
Introduction 77
Double Integration Method 77 – 78
Area Moment Method 78 – 79
Maxwell’s Law of Reciprocal Deflections 79 – 85
Solved Examples 86 – 94
Assignment – 1 95 – 97
Assignment – 2 98 – 99
Answer keys 100
Explanations 100 – 105
#5. Torsion 106 - 133
Introduction 106
Torsion 106 - 107
Torsion of Shafts 108 – 109
Combined Bending and Torsion 109 – 110
Solved Examples 111 – 118
Assignment – 1 119 – 122
Assignment – 2 123 – 124
Answer keys 125
Explanations 125 - 133
#6. Mohr’s Circle 134 - 150
Introduction 134
Mohr’s Circle 134 – 135
Applications : Thin – Walled Pressure Vessel 135 – 136
Solved Example 137 – 141
Assignment – 1 142 – 144
Assignment – 2 145 – 147
Answer key 148
Explanation 148 – 150
#7. Strain Energy Method 151 - 163
Introduction 151
Elastic strain Energy in Uniaxial Loading 151
Elastic strain Energy in Flexural Loading 151 – 152
Elastic strain Energy in Torsional Loading 152
Castigliano’s Theorem 152
Content SOM
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Impact or Dynamic Loading 152 - 153
Solved Examples 154 – 157
Assignment – 1 158 – 159
Assignment – 2 159 – 160
Answer keys 161
Explanations 161 – 163
#8. Columns and Struts 164 – 180
Introduction 164
Columns & Struts 164 – 165
Euler’s Theory of Buckling 165 – 166
Effective Length of Columns 166 – 167
Limitations of Euler’s Formula 167
Rankine’s Formula 168
Solved Examples 169 – 174
Assignment – 1 175 – 176
Assignment – 2 176 – 177
Answer keys 178
Explanations 178– 180
Module Test 181 – 205
Module Test 181 – 191
Answer keys 192
Explanations 192 – 205
Reference 206
Chapter 1 SOM
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CHAPTER 1
Simple Stress and Strain
Introduction
Strength of materials deals with the elastic behavior of materials and the stability of members. The concept of strength of materials is used to determine the stress and deformation of axially loaded members, connections, torsion members, thin-walled pressure vessels, beams, eccentrically loaded members and columns. In this chapter we will study the stress and strain due to axial loading, temperature change and thin walled pressure vessels.
Simple Stress & Strain
Stress is the internal resistance offered by the body per unit area. Stress is represented as force per unit area. Typical units of stress are N/m2, ksi and MPa. There are two primary types of stresses: normal stress and shear stress. Normal stress, is calculated when the force is normal to the surface area whereas the shear stress is calculated when the force is parallel to the surface area.
normal to areaPσ=
A
parallel to areaPτ=
A
Linear strain (normal strain, longitudinal strain, axial strain is a change in length per unit length. Linear strain has no units. Shear strain is an angular deformation resulting from shear stress. Shear strain may be presented in units of radians, percent or no units at all.
δÎ=
L
parallelδ
γ= =tanθ»θHeight
[ in radians]
Hooke’s Law: Axial and Shearing Deformations
Hooke‘s law is a simple mathematical relationship between elastic stress and strain: Stress is proportional to strain. For normal stress, the constant of proportionality is the modulus of elasticity (Young’s Modulus) E.
E
Chapter 1 SOM
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The deformation δ of an axially loaded member of original length L can be derived from Hooke’s
law. Tension loading is considered to be positive, compressive loading is negative. The sign of
the deformation will be the same as the sign of the loading.
AE
PL
ELL
This expression for axial deformation assumes that the linear strain is proportional to the
normal stress E and that the cross-sectional area is constant.
When an axial member has distinct sections differing in cross-sectional area or composition,
superposition is used to calculate the total deformation as the sum of individual deformations.
AE
LP
AE
PL
When one of the variables (e.g., A), varies continuously along the length,
AE
dLP
AE
PdL
The new length of the member including the deformation is given by
LL f
The algebraic deformation must be observed.
Hooke’s law may also be applied to a plane element in pure shear. For such an element, the shear
stress is linearly related to the shear strain, by the shear modulus (also known as the modulus of
rigidity), G.
G
The relationship between shearing deformation, s and applied shearing force, V is then
expressed by
AG
VLs
Chapter 1 SOM
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Stress-Strain Diagram
Proportional Limit: It is the point on the stress strain curve up to which stress is proportional to strain.
Elastic Limit: It is the point on the stress strain curve up to which material will return to its original shape when unloaded.
Yield Point: It is the point on the stress strain curve at which there is an appreciable elongation or yielding of the material without any corresponding increase of load indeed the load actually may decrease while the yielding occurs.
Ultimate Strength: It is the highest ordinate on the stress strain curve.
Rupture Strength: It is the stress at failure
Modulus of Resilience
The work done on a unit volume of material, as a simple tensile force is gradually increased from zero to such a value that the proportional limit of the material is reached, is defined as the modulus of resilience. This may be calculated as the area under the stress-strain curve from the origin up to the proportional limit
Modulus of Toughness The work done on a unit volume of material as a simple tensile force is gradually increased from zero to the value causing rupture is defined as the modulus of toughness. This may be calculated as the entire area under the stress-strain curve from the origin to rupture. Toughness of a material is its ability to absorb energy in the plastic range of the material.
Stress
ς P
A
Yield point
Elastic limit
Proportional limit
Rupture
strength
Ultimate strength
Actual rupture
strength
0 Strain
δ
L
Chapter 1 SOM
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Percentage Elongation
The increase in length of a bar after fracture divided by the initial length and multiplied by 100 is the percentage elongation. Both the percentage reduction in area and the percentage elongation are considered to be measures of the ductility of a material.
Strain Hardening
If a ductile material can be stressed considerably beyond the yield point without failure, it is said to strain-harden. This is true of many structural metals.
Poisson’s Ratio: Biaxial and Triaxial Deformations
Poisson’s ratio , is a constant that relates the lateral strain to the axial strain for axially loaded members.
axial
lateral
Theoretically Poisson’s ratio could vary from zero to 0.5, but typical values are 0.33 for aluminum and 0.3 for steel and maximum value of 0.5 for rubber.
Poisson’s ratio permits us to extend Hooke’s law of uniaxial stress to the case of biaxial stress. Thus if an element is subjected simultaneously to tensile stresses in x and y direction, the strain in the x direction due to tensile stress x is x/E. Simultaneously the tensile stress y will produce lateral contraction in the x direction of the amount y/E, so the resultant unit deformation or strain in the x direction will be
EE
yxx
Similarly, the total strain in the y direction is
EE
xy
y
Hooke’s law can be further extended for three-dimensional stress-strain relationships and written in terms of the three elastic constants, E, G and . The following equations can be used to find the strains caused due to simultaneous action of triaxial tensile stresses:
zyxxE
1
xzyyE
1
yxzzE
1
Chapter 1 SOM
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G
xy
xy
G
yz
yz
G
zxzx
For an elastic isotropic material, the modulus of elasticity E, shear modulus G and Poisson’s ratio are related by
12
EG
12GE
The bulk modulus (K) describes volumetric elasticity or the tendency of an object's volume to deform when under pressure; it is defined as volumetric stress over volumetric strain, is the inverse of compressibility. The bulk modulus is an extension of Young's modulus to three dimensions.
For an elastic, isotropic material, the modulus of elasticity E, bulk modulus K, Poisson’s ratio are related by
21K3E
Thermal stresses
Temperature causes bodies to expand or contract. Change in length due to increase in temperature can be expressed as
L L. . t
Where, L is the length, (/oC) is the coefficient of linear expansion, t (oC) is the temperature change.
From the above equation thermal strain can be expressed as:
If a temperature deformation is permitted to occur freely no load or the stress will be induced in the structure. But in some cases it is not possible to permit these temperature deformations, which results in creation of internal forces that resist them. The stresses caused by these internal forces are known as thermal stresses.
When the temperature deformation is prevented, thermal stress developed due to temperature change can be given as:
ς E. . t
Cylindrical Pressure Vehicle
Hoop Stress : A pressure vessel is a container that holds a fluid (liquid or gas) under pressure. Examples include carbonated beverage bottles, propane tanks and water supply pipes. In a small pressure vessel such as a horizontal pipe, we can ignore the effects of gravity on the fluid. If the