Course in Nonlinear Finite Element Analysis -...

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Plasticity I Computational Mechanics, AAU, Esbjerg Nonlinear Finite Element Analysis Course in Nonlinear Finite Element Analysis Plasticity I

Transcript of Course in Nonlinear Finite Element Analysis -...

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Course in Nonlinear Finite Element Analysis

Plasticity I

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Types of structural nonlinearity classifications used in engineering problems

• Geometric nonlinearity• Material nonlinearity:

– time-independent behaviour such as plasticity– time-dependent behaviour such as creep– viscoelastic/viscoplastic behaviour where both

plasticity and creep effects occur simultaneously

• Contact or boundary nonlinearity

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Strain RateStrain Rate effects:

If a specimen is held at constant strain, the stress will relax slowly. If the straining is resumed, the specimen will behave as though the solid were unloaded elastically. If the specimen is held at constant stress, the specimen will undergo slow, irreversible deformation, i.e. creep.

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Nonlinear Material Response

1. Nonlinear Elastic2. Plastic3. Viscoelastic4. Viscoplastic

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

σ

εO

Loading andunloading

Nonlinear Elastic

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

σ

εO

Loading

Plastic A

B

Unloading

PermanentStrain

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

σ

εO

Loading

Viscoelastic

A

B

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

σ

εO

Loading

Viscoplastic

A

B

Unloading

PermanentStrain

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Idealized Behavior

1. Elastic-perfectly plastic response2. Elastic-strain hardening response3. Rigid elastic -perfectly plastic response4. Rigid elastic -strain hardening response

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

σ

εA A ′

B C F

D

C′F′H

YElasticElastic--Perfectly Perfectly Plastic BehaviorPlastic Behavior

Loading

Loading

Unloading(elastic)

Unloading(elastic)

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

σ

εA A′

BC

F

D

C′F′H

YElastic Elastic

StrainStrain--HardeningHardeningBehaviorBehavior

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

σ

εA A′

B C F

D

C′F′H

YRigid ElasticRigid Elastic--

Perfectly Plastic Perfectly Plastic BehaviorBehavior

Continued Loading(Plastic)

Unloading(Elastic)

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

σ

εA A′

BC F

D

C′F′ H

YRigid ElasticRigid Elastic--

StrainStrain--Hardening Hardening Plastic BehaviorPlastic Behavior

Continued Loading(Plastic)

Unloading(Elastic)

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Plasticity Theory

• Yield criterion or yield function, i.e. defines the state of stress at which material response changes from elastic to plastic.

• Flow rule, i.e. relates plastic strain increments to stress increments after the onset of initial yielding.

• Hardening rule, i.e. predicts the change in the yield surface due to plastic strains.

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Yield criteria• Maximum principal stress criterion or Rankine’s criterion, i.e.

Yielding begins at a point in a member when the maximum principal stress reaches a value equal to the tensile (or compressive) yield stress in uniaxial tension (or compression)

• Maximum principal strain criterion or St. Venant’s criterion, i.e. yielding begins at a point in a member when the maximum principal strain reaches a value equal to the yield strain in uniaxial tension

• Strain energy density criterion, i.e. yielding occurs when the strain energy density is equal to strain energy density at yield for the uniaxial case

• Maximum shear-stress criterion or Tresca’s criterion, i.e. yielding occurs when the maximum shear stress reaches the value of the maximum shear stress at yield in uniaxial tension

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Yield criteria• Distortional energy density or von Mises criterion

(Huber, Maxwell, Hencky), i.e. yielding occurs when the distortional energy density reaches a value equal to the distortional energy density at yield in a uniaxial case.

• Mohr-Coulomb criterion, i.e. generalized form of the Tresca criterion where the limiting shear stress is not constant, but depends on the normal stress

• Drucker-Prager yield criterion, i.e. generalization of von Mises criterion

• Hill’s criterion for orthotropic materials

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Yield Criterion

Define a yield function F, which is a function of stresses {σ} and parameters {α} and Wp associated with the hardening rule.

{ } { }( )( ) 0W,,F

0W,,F

p

p

=ασ

=ασ

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Yield Criterion

Possible values of F:F < 0 - elastic rangeF = 0 - yieldingF > 0 - impossible

Possible values of dF:dF < 0 - unloadingdF = 0 - continued yieldingdF > 0 - impossible

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Yield Criterion

1. Defines the onset of yielding2. |σ| = σy

3. σy - yield stress in uniaxial tension4. Tresca5. von Mises

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Flow Rule

Define a plastic potential Q, which is a function of

stresses {σ} and parameters {α} and Wp

associated with the hardening rule. Also define

a scalar dλ that may be called a “plastic

multiplier.” Plastic strain increments are given by:

{ } { }( )

{ } { } λ⎭⎬⎫

⎩⎨⎧

σ∂∂

ασ=

dQd

W,,QQ

p

p

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Flow Rule

λσ∂∂=γ

λσ∂∂=ε

λσ∂∂=ε

dQd

dQd

dQd

xz

pxz

y

py

x

px

M

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Flow Rule

(soils) materials granular rule - flow tednonassociamaterialsductile rule - flow associated

rule. flow tednonassociarule. flow associated

FQFQ

≠=

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Flow Rule

1. Relates stress increment {dσ} to strain increment {dε} after yielding.

2. Uniaxial case: dσ = Et dε3. Prandtl-Reuss often used.4. Associated - ductile materials.5. Non-associated - soil or granular

materials.

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Hardening Rule• If an unloading is followed by a reversed loading, e.g.

tension is followed by compression, metals exhibit yielding at lower load than was the original yield limit. This is termed the Bauschinger effect.

• In a general multi-axial stress state, the hardening phenomena correspond to change in the size/shape and/or translation of the original elastic domain. This phenomenon is often simplified by assuming that the elastic domain does not change in shape, but only uniformly expands (isotropic hardening) or translates (kinematic hardening) or expands and translates (mixed hardening) in the stress space.

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Hardening Rule

Basically two hardening rules exist:

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Hardening Rule

The parameter {α} locates the center of the yield surface in stress space. Before any yielding occurs {α} = 0. In kinematic hardening the yield surface moves in the direction of plastic straining, so {α}≠ 0. The parameter Wp describes how the yield surface grows. For isotropic hardening, {α} = 0 throughout the analysis and Wp ≠ 0.

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Hardening Rule

The parameters {α} and Wp are given by:

{ } { }{ } { }∫∫

εσ=

ε=α

pTp

p

dW

dC

Where C can be assumed to be a material constant.

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Hardening Rules

1. Kinematic1. Yield surface retains size and shape and

translates in stress space.2. Isotropic

1. Yield surface retains shape but increases in size.

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

ε

σ

B

YσE E

Y2σ

tE

tE

tE

Kinematic

Isotropic

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Yield Surface

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Yield Surface

Isotropic Hardening

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Yield Surface

Kinematic Hardening

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Maximum Principal Strain Criterion

Also known as St. Venant’s criterion.

Yielding begins at a point in a member when the maximum principal strain reaches a value equal to the yield strain in uniaxial tension.

EYεY =

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Assume a uniaxial case where σ1 is the only non-zero principal stress. Yielding occurs when :

1 Y 1Y YE

ε = ε = ⇒ σ =

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

2σ2σ

Assume a case where two principal stresses σ1 and σ2 both act. Yielding occurs when ε1=Y

21 σ≥σ

⎟⎠⎞

⎜⎝⎛ σν−⎟

⎠⎞

⎜⎝⎛ σ=ε

EE21

1

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

2σ2σ

σ2 >0 Yielding occurs at σ1 >Y

σ2 <0 Yielding occurs at σ1 <Y

21 σ≥σ

⎟⎠⎞

⎜⎝⎛ σν−⎟

⎠⎞

⎜⎝⎛ σ=ε

EE21

1

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

( )

YY

E1ε

ε

321

321

3211

1

±=νσ−νσ−σ

−νσ−νσ−σ=

νσ−νσ−σ=

1f

strain principal largestthe is Assume

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

( )

( )

( ) YYE1ε

YYE1ε

YYE1ε

2132132133

3123123222

3213213211

±=νσ−νσ−σ−νσ−νσ−σ=νσ−νσ−σ=

±=νσ−νσ−σ−νσ−νσ−σ=νσ−νσ−σ=

±=νσ−νσ−σ−νσ−νσ−σ=νσ−νσ−σ=

3

2

1

f

f

f

unorderedare strain principalAssume

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Y

max

−σ=

νσ−νσ−σ=σ≠≠

e

kjie

f

kji

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Yσ1 =

Yσ1 −=

Yσ2 =

Yσ2 −=

Yσ 12 =νσ−

Yσ 21 =νσ−

Yσ 21 −=νσ−

Yσ 12 −=νσ−A

BC

D

Maximum Principal Strain

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Strain Energy Density Criterion

Proposed by Beltrami states that yielding occurs when the strain energy density is equal to strain energy density at yield for the uniaxial case.

( )2 2 20 1 2 3 1 2 1 3 2 3

1U 2 02E

⎡ ⎤= σ +σ +σ − ν σ σ +σ σ +σ σ >⎣ ⎦

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Strain Energy Density Criterion

( )[ ]

[ ]E2

YE2

1U

0Y

2E2

1U

2210

321

32312123

22

210

=σ=

=σ=σ=σ

σσ+σσ+σσν−σ+σ+σ=

:case Uniaxial

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Strain Energy Density Criterion

( )

( )

22 2 21 2 3 1 2 1 3 2 3

2 2 2 21 2 3 1 2 1 3 2 3

1 Y2 02 E 2 E

2 Y 0

σ + σ + σ − ν σ σ + σ σ + σ σ − =

σ + σ + σ − ν σ σ + σ σ + σ σ − =

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Strain Energy Density Criterion

( )

( )

2 2e

2 2 2e 1 2 3 1 2 1 3 2 3

f σ Y

σ 2

= −

= σ + σ + σ − ν σ σ + σ σ + σ σ

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Biaxial Case

( ) 0Y2 221

22

21 =−σσν−σ+σ

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Maximum Shear-Stress Criterionor Tresca Criterion

Yielding occurs when the maximum shear stress reaches the value of the maximum shear stress at yield in uniaxial tension.

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Uniaxial Loading

2Y

20Y

0σ0σYσ

max

3

2

1

=−

===

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Tresca Criterion

maxe

e

σ2Yσ

τ=

−=f

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Tresca Criterion

( )321max

213

132

321

,,max2

2

2

τττ=τ

σ−σ=τ

σ−σ=τ

σ−σ=τ

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Tresca Criterion

YYY

21

13

32

±=σ−σ±=σ−σ±=σ−σ

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Yσ1 =

Yσ1 −=

Yσ2 =

Yσ2 −=

Y

D

Yσ 21 =σ−

Y

Y−

Y−

Yσ 21 −=σ−

Tresca

0σ3 =

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Distortional Energy Density von Mises Criterion

Yielding occurs when the distortional energy density reaches a value equal to the distortional energy density at yield in a uniaxial case.

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Strain Energy Density

( )2 2 20 1 2 3 1 2 1 3 2 3

0 V D

1U 22E

U U U

⎡ ⎤= σ + σ + σ − ν σ σ + σ σ + σ σ⎣ ⎦

= +

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Strain Energy Density

( )

( ) ( ) ( )

21 2 3

V

2 2 21 2 2 3 3 1

D

σ σ σU

18K

U12G

+ +=

σ − σ + σ − σ + σ − σ=

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Strain Energy Density

( )EK

3 1 2 ν

Bulk Modulus

=−

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Strain Energy Density

( )EG

2 1 ν

Shear Modulus

=+

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Distortional StrainEnergy Density

( ) ( ) ( )G12

213

232

221 σ−σ+σ−σ+σ−σ

=DU

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Uniaxial Loading

( ) ( ) ( )1 2 3

2 2 2

D

2

D

σ Y σ 0 σ 0

Y 0 0 0 0 YU

12GYU6G

= = =

− + − + −=

=

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Deviatoric Stress

⎥⎥⎥⎥

⎢⎢⎢⎢

=

m

m

m

dT

σσσσ

σσσσ

σσσσ

zzzyzx

yzyyyx

xzxyxx

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

( ) ( ) ( )[ ]

( )( )( )213132321271

3127

2213

133

213

232

2216

1

213

122

1

σσσ2σσσ2σσσ2

σσσσσσ

0

−−−−−−=

++=

−+−+−=

+=

=

IIIIJ

IIJ

J

Deviatoric Stress Invariants

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

von Mises Criterion

( ) ( ) ( )G2

JG12

22

132

322

21 =σ−σ+σ−σ+σ−σ

=DU

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

von Mises Criterion

( ) ( ) ( )2 2 2 21 2 2 3 3 1 Y

12G 6G

22

1J Y3

σ − σ + σ − σ + σ − σ=

=

Plasticity IComputational Mechanics, AAU, EsbjergNonlinear Finite Element Analysis

Von Mises Criterion

( ) ( ) ( )

( ) ( ) ( )

2 2 2 21 11 2 2 3 3 16 3

2 2e

2 2 21e 1 2 2 3 3 1 22

Y

σ Y

3J

f

f

⎡ ⎤= σ − σ + σ − σ + σ − σ −⎣ ⎦

= −

⎡ ⎤σ = σ − σ + σ − σ + σ − σ =⎣ ⎦