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FORMULA SHEET FOR ENGINEERING 3016 PART 4 – MECHANICS OF MATERIALS Chapter 4 Stress, Strain, and Deformation: Axial Loading Normal stress is normal to the plane F A σ = , is the normal force, F A is the cross-sectional area. Shear stress is in the plane V A τ = , is the shear force, V A is the cross-sectional area. Average normal strain n L δ ε = Average shear strain tan s L δ γ φ = = Hooke’s Law: for normal stress E σ ε = for shear stress G τ γ = E is the Young’s modulus G is the shear modulus 2(1 ) E G ν = + , lat long ε ν ε =− is Poisson’s ratio where lat ε is strain in lateral direction and long ε is strain in longitudinal direction. . Deformation of Axially Loaded Members Member with uniform cross section PL EA δ = Members with multiple loads/sizes 1 n i i i i i PL EA δ = = Stress-Strain Relationships Low-carbon steel or ductile materials High-carbon steel or alloy steel 1

Formula Sheet Mechanics Materials

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Page 1: Formula Sheet Mechanics Materials

FORMULA SHEET FOR ENGINEERING 3016 PART 4 – MECHANICS OF MATERIALS

Chapter 4 Stress, Strain, and Deformation: Axial Loading

Normal stress is normal to the plane FA

σ = , is the

normal force,

F

A is the cross-sectional area.

Shear stress is in the plane VA

τ = , is the shear

force,

V

A is the cross-sectional area.

Average normal strain n

Lδε =

Average shear strain tans

Lδγ φ= =

Hooke’s Law: for normal stress Eσ ε= for shear stress Gτ γ= E is the Young’s modulus G is the shear modulus

2(1 )EGν

=+

, lat

long

ενε

= − is Poisson’s ratio where latε

is strain in lateral direction and longε is strain in longitudinal direction. . Deformation of Axially Loaded Members

Member with uniform cross section PLEA

δ =

Members with multiple loads/sizes 1

ni i

i i i

PLE A

δ=

=∑

Stress-Strain Relationships Low-carbon steel or ductile materials

High-carbon steel or alloy steel

1

Page 2: Formula Sheet Mechanics Materials

Chapter 7 Torsional Loading: Shafts

Shear stress at c, Tc

Jτ = ,

J is polar second moment of area

For solid cross section 4

2J cπ=

For hollow cross section 4 42 1( )

2J c cπ= −

Torsional displacement or angle of twist

For uniform shaft TLGJ

θ =

For shaft with multi-step 1

ni i

i i i

T LG J

θ=

=∑

Work of a couple u Cθ= , is couple, C θ is angle of twist Power Transmission by Torsional Shafts Power Tω= , ω is angular velocity

Chapter 8 Flexural Loading: Stress in Beams

rM is the resultant of normal stress

rV is the resultant of shear stress The Elastic Flexural Formula

Normal stress at : y MyI

σ = −

Max. normal stress at upper surface y c= : rM cI

σ = −

I is the second moment of area For a rectangular cross section

For a circular cross section

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Page 3: Formula Sheet Mechanics Materials

Shear Forces and Bending Moments in Beams

the max. bending stress maxmax

rMS

σ = where ISc

= is

the section modulus of the beam. If the beam is uniform cross section, S is constant.

maxrM is the max. bending moment in the beam as rM varies along the beam, to find , need to draw the bending moment diagram.

maxrM

Shear force diagram shows the variation of the shear force along beam rVBending moment diagram shows the variation of the bending moment rM along beam Sign convention

Procedure 1. Find the reactions at supports. 2. Determine how to divide the beam into different

segments. 3. Starting from the far left end, section the beam at

an arbitrary location x within the chosen segment. 4. Draw FBD for the portion of the beam to the left. 5. Apply equilibrium equations. 6. Repeat the process for each different segment of

the beam.

Chapter 9 Flexural Loading: Beam Deflections

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Page 4: Formula Sheet Mechanics Materials

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