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EAT203 Lecture 1: Stress-strain relationship

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Page 1: Lecture+1+-+Stress-strain+relationship

EAT203Lecture 1: Stress-strain relationship

Page 2: Lecture+1+-+Stress-strain+relationship

EAT203, Engineering Mechanics

Lecture Topic Tutorial

1 Stress-strain relationship2 Shear force (SF) and bending moment (BM) for non-uniform loading 13 SF and BM for statically indeterminate problem4 Shear stress in bending 25 Stress transformation6 Experimental stress / strain 37 Yield criteria (theories of failure)8 Stress concentration + Fatigue 49 Vibration (Forced with damping) 510 Kinematics - particle (velocity diagram)11 Kinematics - ridig body (velocity diagram)12 Kinematics - acceleration diagram 613 Gear system14 Balancing of rotating system 7

[1] Benham, P.P., Crawford, R.J. & Armstrong, C.G., Mechnics of Engineering Materials, 2nd ed., Prentice Hall, UK (1996)[2] Hibbeler, R. C., Mechanics of Materials, 7th ed., Prentice Hall, Singapore (2008)[3] Hibbeler, R. C., Engineering Mechanics Dynamics, 8th ed., Prentice-Hall International

Page 3: Lecture+1+-+Stress-strain+relationship

Stress

• The effect of external applied forces on a solid body or the member of a framework can be measured in terms of the internal reacting forces.

• The intensity of internal force at a point is called stress.

• Stress is defined as the internal force per unit cross section area at right angle to the direction of the force.

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Average Normal Stress Distribution

When a bar is subjected to a constant deformation

APAP

dAdFA

σ = average normal stressP = resultant normal forceA = cross sectional area of bar

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Shear Stress, • If an applied load consists of two equal and opposite

forces which are not in the same line, then the material being loaded will tend to shear as shown.

• Shear stress is the force (acting tangent to the area) per unit area

AF

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StrainDirect strain

• Consider a uniform bar subjected to an axial tensile load, F. If the resulting extension of the bar is and its unloaded (original) length is L, then the direct tensile strain is

L

Page 7: Lecture+1+-+Stress-strain+relationship

Shear strain• A shear stress produces a shear strain as is

shown below. The shear strain is defined as• For small deflection,

• The shear strain is dimensionless and is measured in radians

yx tan

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Example 1The plate is deformed into the dashed shape. If, in this deformed shape, horizontal lines on the plate remain horizontal and do not change their length, determine (a) the average normal strain along the side AB, and (b) the average shear strain in the plate relative to the x and y axes.

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Line AB, coincident with the y axis, becomes line AB’ after deformation, thus the length of this line is

The average normal strain for AB is

The negative sign indicates the strain causes a contraction of AB.

Solution: Part (a)

mm 018.24832250' 22 AB

(Ans) 1093.7250

250018.248'

3

ABABAB

avgAB

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As noted, the once 90°angle BAC between the sides of the plate, referenced from the x, y axes, changes to θ’ due to the displacement of B to B’.

Since then is the angle shown in the figure.

Solution: Part (b)

'2 xy xy

(Ans) rad 0121.02250

3tan 1

xy

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Page 12: Lecture+1+-+Stress-strain+relationship

G

Hooke’s Law defines the linear relationship between the normal stress and strain within the elastic region, i.e., Young’s modulus.

Eσ = normal stressE = Young’s modulusε = normal strain

While Young’s modulus describe the material’s response to direct strain, shear modulus, G describe the material’s response to shear strain

vGEand 12

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• states that in the elastic range, the lateral strain is proportional to the direct strain (due to stress), where

• Negative sign, as direct strain (negative) causes lateral expansion (positive strain), and vice versa.

• Typical values for Poisson’s ratio are 1/3 or 1/4.

direct

lateralv

Poisson’s Ratio, v

Page 14: Lecture+1+-+Stress-strain+relationship

Example 2

A steel bar (E = 210GPa, v = 0.32) has the dimensions shown. If an axial force of is applied to the bar, determine the change in its length and the change in the dimensions of its cross section after applying the load. The material behaves elastically.

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Solution:

The normal stress in the bar is

69

6

107610210100.16

st

zz E

Pa 100.16

05.01.01080 6

3

AP

z

The axial elongation of the bar is therefore

(Ans) m1145.11076 6z

zz L

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The contraction strains in x and y directions are

-66 103.24107632.0 zstyx v

The changes in the dimensions of the cross section are (Ans) m215.105.0103.24

(Ans) m43.21.0103.246

6

yyy

xxx

L

L

Page 17: Lecture+1+-+Stress-strain+relationship

zyx

zyxx

Ev

E

Ev

Ev

E

zxy

y Ev

E

3D stress-strain

xyz

z Ev

E

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yzyxy vE

vvvE

1211

xzyxx vE

vvvE

1211

zzyxz vE

vvvE

1211

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Plane stress

Ev

Eyx

x

Ev

Exy

y

yxz Ev

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Coefficient of Linear Thermal Expansion

• Most materials increase in volume as their temperature increases

• Change in length of a structural member of length L is proportional to temperature increase T:

= .T.L

• Constant of proportionality (K-1) is coefficient of linear thermal expansion {C.T.E.}

Page 21: Lecture+1+-+Stress-strain+relationship

• Increasing temperature causes expansion and thus a positive strain and vice versa.

• Then thermal strain, = /L = .T

L

A B

Unconstrained Bar

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Axial Stress in Constrained Bar• If there is any restriction on the material, then a

thermal stress will result. For an initially unstressed prismatic bar AB, an axial stress (F) developed as it undergoes an increase in temperature.

L

L

F

A

A

B

B

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• In this case, principle of superposition is to be applied

• Within elastic limit, assess effects of temperature change and load separately

• Add results, noting sign, to determine total effect, i.e. total strain = sum of strains due to both external loads and thermal strains

Total strain, = strain due to external load, F + thermal strain

0 = -(F/EA) + .T

F = .T.E.A

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Example 3

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