failure theories - static loads

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1 Static load – a stationary load that is gradually applied having an unchanging magnitude and direction Failure – A part is permanently distorted and will not function properly. A part has been separated into two or more pieces. Material Strength S y = Yield strength in tension, S yt = S yc S ys = Yield strength in shear S u = Ultimate strength in tension, S ut S uc = Ultimate strength in compression S us = Ultimate strength in shear = .67 S u

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Page 1: Failure Theories - Static Loads

1

Static load – a stationary load that is gradually applied having an unchanging magnitude and direction

Failure – A part is permanently distorted and will not function properly.

A part has been separated into two or more pieces.

Material Strength

Sy = Yield strength in tension, Syt = Syc

Sys = Yield strength in shear

Su = Ultimate strength in tension, Sut

Suc = Ultimate strength in compression

Sus = Ultimate strength in shear = .67 Su

Page 2: Failure Theories - Static Loads

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A ductile material deforms significantly before fracturing. Ductility is measured by % elongation at the fracture point. Materials with 5% or more elongation are considered ductile.

Brittle material yields very little before fracturing, the yield strength is approximately the same as the ultimate strength in tension. The ultimate strength in compression is much larger than the ultimate strength in tension.

Page 3: Failure Theories - Static Loads

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• Maximum shear stress theory (Tresca 1886)

Yield strength of a material is used to design components made of ductile material

σ = Sy

τSy

2=

σ = Sy

σ =Sy

(τmax )component > (τ )obtained from a tension test at the yield point Failure

(τmax )component < Sy

2

To avoid failure

τmax = Sy

2 nn = Safety factor

Design equation

Page 4: Failure Theories - Static Loads

4

• Distortion energy theory (von Mises-Hencky)

Hydrostatic state of stress → (Sy)h

σh

σh

σh

σt

σt

Simple tension test → (Sy)t

(Sy)t(Sy)h >>

Distortion contributes to failure much more than change in volume.

(total strain energy) – (strain energy due to hydrostatic stress) = strain energy due to angular distortion > strain energy obtained from a tension test at the yield point → failure

Page 5: Failure Theories - Static Loads

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The area under the curve in the elastic region is called the Elastic Strain Energy.

Strain energy

U = ½ σε

3D case

UT = ½ σ1ε1 + ½ σ2ε2 + ½ σ3ε3

ε1 = σ1

E

σ2

E

σ3

Evv

ε2 = σ2

E

σ1

E

σ3

Evv

ε3 = σ3 σ1

E

σ2

Evv

Stress-strain relationship

E

UT = (σ12 + σ2

2 + σ32) - 2v (σ1σ2 + σ1σ3 + σ2σ3) 2E

1

Page 6: Failure Theories - Static Loads

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Ud = UT – Uh

Distortion strain energy = total strain energy – hydrostatic strain energy

Substitute σ1 = σ2 = σ3 = σh

Uh = (σh2 + σh

2 + σh2) - 2v (σhσh + σhσh+ σhσh) 2E

1

Simplify and substitute σ1 + σ2 + σ3 = 3σh into the above equation

Uh = (1 – 2v) =2E

3σh2

6E

(1 – 2v)(σ1 + σ2 + σ3)2

Ud = UT – Uh = 6E

1 + v(σ1 – σ2)

2 + (σ1 – σ3)2 + (σ2 – σ3)

2

Subtract the hydrostatic strain energy from the total energy to obtain the distortion energy

UT = (σ12 + σ2

2 + σ32) - 2v (σ1σ2 + σ1σ3 + σ2σ3) 2E

1 (1)

(2)

Page 7: Failure Theories - Static Loads

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Strain energy from a tension test at the yield point

σ1= Sy and σ2 = σ3 = 0 Substitute in equation (2)

3E

1 + v(Sy)

2Utest =

To avoid failure, Ud < Utest

(σ1 – σ2)2 + (σ1 – σ3)

2 + (σ2 – σ3)2

2

½ < Sy

Ud = UT – Uh = 6E

1 + v(σ1 – σ2)

2 + (σ1 – σ3)2 + (σ2 – σ3)

2 (2)

Page 8: Failure Theories - Static Loads

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½

2D case, σ3 = 0

(σ12 – σ1σ2 + σ2

2) < Sy = σ′Where σ′ is von Mises stress

σ′ = Sy

nDesign equation

(σ1 – σ2)2 + (σ1 – σ3)

2 + (σ2 – σ3)2

2

½ < Sy

Page 9: Failure Theories - Static Loads

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Pure torsion, τ = σ1 = – σ2

(σ12 – σ2 σ1 + σ2

2) = Sy2

3τ2 = Sy2

Sys = Sy / √ 3 → Sys = .577 Sy

Relationship between yield strength in tension and shear

(σx)2 + 3(τxy)

2 =

Sy

n

1/2

If σy = 0, then σ1, σ2 = σx/2 ± [(σx)/2]2 + (τxy)2

the design equation can be written in terms of the dominant component stresses (due to bending and torsion)

Page 10: Failure Theories - Static Loads

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σ′ = Sy

nτmax =

Sy

2n

Maximum shear stress theoryDistortion energy theory

• Select material: consider environment, density, availability → Sy , Su

• Choose a safety factor

The selection of an appropriate safety factor should be based on the following:

Degree of uncertainty about loading (type, magnitude and direction)

Degree of uncertainty about material strength

Type of manufacturing process

Uncertainties related to stress analysis

Consequence of failure; human safety and economics

Codes and standards

n CostWeightSize

Page 11: Failure Theories - Static Loads

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Use n = 1.2 to 1.5 for reliable materials subjected to loads that can be determined with certainty.

Use n = 1.5 to 2.5 for average materials subjected to loads that can be determined. Also, human safety and economics are not an issue.

Use n = 3.0 to 4.0 for well known materials subjected to uncertain loads.

Page 12: Failure Theories - Static Loads

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• Formulate the von Mises or maximum shear stress in terms of size.

• Optimize for weight, size, or cost.

• Select material, consider environment, density, availability → Sy , Su

• Choose a safety factor

• Use appropriate failure theory to calculate the size.

σ′ = Sy

nτmax =

Sy

2n

Page 13: Failure Theories - Static Loads

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One of the characteristics of a brittle material is that the ultimate strength in compression is much larger than ultimate strength in tension.

Suc >> SutMohr’s circles for compression and tension tests.

Compression test

Suc

Failure envelope

The component is safe if the state of stress falls inside the failure envelope.

σ1 > σ3 and σ2 = 0

Tension test

σ

τ

Sutσ3 σ1Stress state

Page 14: Failure Theories - Static Loads

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σ1

Sut

Suc

Sut

Suc

Safe

Safe

Safe Safe

-Sut

Cast iron data

Modified Coulomb-Mohr theory

σ1

σ3 or σ2

Sut

Sut

Suc

-Sut

I

II

III

Three design zones

σ3 or σ2

Page 15: Failure Theories - Static Loads

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σ1

σ3

Sut

Sut

Suc

-Sut

I

II

III

Zone I

σ1 > 0 , σ2 > 0 and σ1 > σ2

Zone II

σ1 > 0 , σ2 < 0 and σ2 < Sut

Zone III

σ1 > 0 , σ2 < 0 and σ2 > Sut σ1 (1

Sut

1

Suc – ) –

σ2

Suc=

1n

Design equation

σ1 =Sut

nDesign equation

σ1 =Sut

nDesign equation