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Explicit-STR_14.0_L06_MaterialModels

Explicit-STR_14.0_L06_MaterialModels
Explicit-STR_14.0_L06_MaterialModels

Lecture 6

Material Models

Introduction to ANSYS Explicit STR

Material Behavior Under Dynamic Loading

In general, materials have a complex response to dynamic loading

The following phenomena may need to be modelled

?Non‐linear pressure response

?Strain hardening

?Strain rate hardening

?Thermal softening

?Compaction (porous materials)

?Orthotropic behavior (e.g. composites)

?Crushing damage (e.g. ceramics, glass, geological materials, concrete)

?Chemical energy deposition (e.g. explosives)

?Tensile failure

?Phase changes (solid‐liquid‐gas)

No single material model incorporates all of these effects

Engineering Data offers a selection of models from which you can choose based on the material(s) present in your simulation

E Modeling Provided By Engineering Data

3

Material Deformation

Material deformation can be split into two independent parts ?Volumetric Response ‐ changes in volume (pressure)

–Equation of state (EOS)

?Deviatoric Response ‐ changes in shape

–Strength model

Also, it is often necessary to specify a Failure model as materials can only sustain limited amount of stress / deformation before they break / crack / cavitate (fluids).

Change in Volume Change in Shape

Principal Stresses

A stress state in 3D can be described by a tensor with six stress components ? Components depend on the orientation of the coordinate system used.

The stress tensor itself is a physical quantity ? Independent of the coordinate system used

When the coordinate system is chosen to coincide with the eigenvectors of the

stress tensor, the stress tensor is represented by a diagonal matrix

where σ1, σ2 , and σ3, are the principal stresses (eigenvalues).

The principal stresses may be combined to form the first, second and third

stress invariants, respectively.

Because of its simplicity, working and thinking in the principal coordinate system

is often used in the formulation of material models.

Elastic Response

?For linear elasticity, stresses are given by Hooke’s law :

where and G are the Lame constants (G is also known as the Shear Modulus)

?The principal stresses can be decomposed into a hydrostatic and a deviatoric component :

where P is the pressure and s i are the stress deviators

?Then :

f

Non‐linear Response

? Many applications involve stresses considerably beyond the elastic limit and so require more complex material models

Hooke ’s Law

Generalized Non-Linear Response

Equation of State

Strength Model

Failure Model

σi (max,min) =

Models Available for Explicit Dynamics

AUTODYN

Equation of State

Strength Model

Failure Model

Elastic Constants

Shear Modulus Young’s Modulus

Shear Modulus Poisson’s Ratio

Shear Modulus Bulk Modulus Young’s Modulus Poisson’s Ratio

Young’s Modulus Bulk Modulus Poisson’s Ratio Bulk Modulus Shear

Modulus G

E

2 (1+ n)

3EK

9K - E

3K (1 - 2n)

2 (1 + n)

Young’s

Modulus E

2G (1 + n)

9KG

3K + G

3K (1 - 2n)

Poisson’s

Ratio n

E - 2G

2G

3K - 2G

2 (3K + G)

3K - E

6K

Bulk

Modulus K

GE

3 (3G - E)

2G (1 + n)

3 (1 - 2n)

E

3 (1 - 2n)

Physical and Thermal Properties

Density

?All material must have a valid density defined for

Explicit Dynamics simulations.

?The density property defines the initial Mass /

unit volume of a material at time zero

–This property is automatically included in all models

Specific Heat

?This is required to calculate the temperature

used in material models that include thermal

softening

–This property is automatically included in thermal

softening models

Linear Elastic

Isotropic Elasticity

?Used to define linear elastic material behavior

– suitable for most materials subjected to low

compressions.

?Properties defined

–Young’s Modulus (E)

–Poisson’s Ratio (ν)

?From the defined properties, Bulk modulus and Shear modulus are derived for use in the material solutions. ?Temperature dependence of the linear elastic

properties is not available for explicit dynamics

Linear Elastic

Orthotropic Elasticity

?Used to define linear orthotropic elastic material behavior

– suitable for most orthotropic materials subjected to low compressions.

?Properties defined

–Young’s Modulii (E x, E y, E z)

–Poisson’s Ratios (νxy, νyz, νxz)

– Shear Modulii (G xy, G yz, G xz)

?Temperature dependence of the properties is not available for explicit dynamics

Linear Elastic

Viscoelastic

?Represents strain rate dependent elastic behavior ?Long term behavior is described by a Long Term Shear Modulus, G∞.

–Specified via an Isotropic Elasticity model or Equation OF State ?Viscoelastic behavior is introduced via an Instantaneous Shear Modulus, G0 and a Viscoelastic Decay Constant β.?The deviatoric viscoelastic stress at time n+1 is calculated from the viscoelastic stress at time n and the shear strain increments at time n:

?Deviatoric viscoelastic stress is added to the elastic stress to give the total stress

Linear Elastic

Viscoelastic

ε= Constant

Stress Strain

Time

Stress Relaxation Creep

Time

Hyperelastic

E n g . S t r e s s (M P a )

Several forms of strain energy potential (Ψ) are

provided for the simulation of nearly incompressible hyperelastic materials.

Forms are generally applicable over different ranges of

strain.

Tensile tests on vulcanised rubber

Mooney-Rivlin Arruda-Boyce O gden

T r eloar Experiments

1

2

3

4 5

6

7

8

Eng. Str a in

Need to verify the applicability of the model chosen

prior to use.

Currently hyperelastic materials may only be used for

solid elements

Hyperelastic

Examples of Hyperelasticity

Plasticity

)

If a material is loaded elastically and subsequently unloaded, all the distortion energy is recovered

and the material reverts to its initial configuration. If the distortion is too great a material will reach its elastic limit and begin to distort plastically.

In Explicit Dynamics, plastic deformation is computed by reference to the Von Mises yield criterion

(also known as Prandtl –Reuss yield criterion) . This states that the local yield condition is

where Y is the yield stress in simple tension. It can be also written as

or

(since

Thus the onset of yielding (plastic flow), is purely a function of the deviatoric stresses (distortion)

and does not depend upon the value of the local hydrostatic pressure unless the yield stress itself is a function of pressure (as is the case for some of the strength models).

Plasticity

If an incremental change in the stresses violates the Von Mises criterion then each of the

principal stress deviators must be adjusted

such that the criterion is satisfied.

If a new stress state n + 1 is calculated from a state n and found to fall outside the yield

surface, it is brought back to the yield

surface along a line normal to the yield

surface by multiplying each of the stress

deviators by the factor

By adjusting the stresses perpendicular to the yield circle only the plastic components of

the stresses are affected.

Effects such as work hardening, strain rate hardening, thermal softening, e.t.c. can be

considered by making Y a dynamic function

of these

Plasticity

Bilinear Isotropic / Kinematic Hardening

?Used to define the yield stress (Y) as a linear function of plastic strain, εp

?Properties defined

– Yield Strength (Y0)

– Tangent Modulus (A)

?Isotropic Hardening

–Total stress range is twice the maximum yield stress, Y ?Kinematic Hardening

–Total stress range is twice the starting yield stress, Y

–Models Bauschinger effect

–Often required to accurately predict response of thin structure (shells)

Plasticity

Isotropic vs Kinematic Hardening

σ

2

σ

2

Current Yield surface

σ

1

σ

1 Initial Yield surface

Isotropic Hardening (σ

3 = 0) Kinematic Hardening (σ

3

= 0)

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