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Lecture Mechanics of materials (Third edition) - Chapter 11: Energy methods

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Strain Energy for a General State of Stress Impact Loading. Example 11.06 Example 11.07[r]

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MECHANICS OF MATERIALS

Ferdinand P Beer

E Russell Johnston, Jr.

John T DeWolf

Lecture Notes:

J Walt Oler Texas Tech University

CHAPTER

Energy Methods

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Strain Energy

Strain Energy Density

Elastic Strain Energy for Normal Stresses

Strain Energy For Shearing Stresses

Sample Problem 11.2

Strain Energy for a General State of Stress

Impact Loading

Example 11.06

Example 11.07

Design for Impact Loads

Work and Energy Under a Single Load

Deflection Under a Single Load

Sample Problem 11.4 Work and Energy Under Several Loads Castigliano’s Theorem

Deflections by Castigliano’s Theorem Sample Problem 11.5

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• A uniform rod is subjected to a slowly increasing load

• The elementary work done by the load P as the rod elongates by a small dx is

which is equal to the area of width dx under the

load-deformation diagram

work elementary

dx P

• The total work done by the load for a deformation x1,

which results in an increase of strain energy in the rod.

energy strain

work total

dx P U

x

=

=

= ∫1

0

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• To eliminate the effects of size, evaluate the strain-energy per unit volume,

density energy

strain d

u

L

dx A

P V

U

x

x

=

=

=

∫ 1 1

0

0

ε

ε σ

• The total strain energy density resulting from the deformation is equal to the area under the curve to ε1

• As the material is unloaded, the stress returns to zero but there is a permanent deformation Only the strain energy represented by the triangular area is recovered

• Remainder of the energy spent in deforming the material

is dissipated as heat

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• The strain energy density resulting from setting ε1 = εR is the modulus of toughness.

• The energy per unit volume required to cause the material to rupture is related to its ductility

as well as its ultimate strength

• If the stress remains within the proportional limit,

E

E d

E

u x

2 2

2 1

2 1 0

1

ε

=

=

= ∫

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• In an element with a nonuniform stress distribution,

energy strain

total

lim

0

=

=

=

dV

dU V

U u

V

• For values of u < u Y, i.e., below the proportional limit,

energy strain

elastic

dV E

2

2

= σ

• Under axial loading, σx = P A dV = A dx

=

L

dx AE

P U

0

2

2

AE

L P U

2

2

=

• For a rod of uniform cross-section,

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y

M

x = σ

• For a beam subjected to a bending load,

EI

y M dV

E

2

2 2 2

2 2

σ

• Setting dV = dA dx,

dx EI M

dx dA

y EI

M dx

dA EI

y M U

L

L

A

L

A

∫ ∫

=

=

=

0

2

0

2 2

2

0

2

2 2

2

2 2

• For an end-loaded cantilever beam,

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• For a material subjected to plane shearing stresses,

=

xy

xy

xy d u

γ

γ τ

0

• For values of τxy within the proportional limit,

G

G

u xy xy xy xy

2

2 2

1 2

2

γ τ

=

• The total strain energy is found from

=

=

dV G

dV u U

xy

2

2

τ

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T

xy

ρ

GJ

T dV

G

U xy

2

2 2 2

2 2

ρ τ

• For a shaft subjected to a torsional load,

• Setting dV = dA dx,

∫ ∫

=

=

=

L

L

A

L

A

dx GJ T

dx

dA GJ

T dx

dA GJ

T U

0

2

0

2 2

2

0

2

2 2

2

2 2

ρ ρ

• In the case of a uniform shaft,

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• Determine the reactions at A and B

from a free-body diagram of the complete beam

• Develop a diagram of the bending moment distribution

a) Taking into account only the normal

stresses due to bending, determine the

strain energy of the beam for the

loading shown

b) Evaluate the strain energy knowing

that the beam is a W10x45, P = 40

kips, L = 12 ft, a = 3 ft, b = 9 ft, and E

= 29x106 psi

• Integrate over the volume of the beam to find the strain energy

• Apply the particular given conditions to evaluate the strain energy

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