An Arbitrary LagrangianEulerian Finite Element Formulation for Dynamics and Finite Strain Plasticity - PowerPoint PPT Presentation

1 / 58
About This Presentation
Title:

An Arbitrary LagrangianEulerian Finite Element Formulation for Dynamics and Finite Strain Plasticity

Description:

Reference configuration M is fixed and independent of any placement of the ... Cut out a part of the body and denote the remaining part as and in the material ... – PowerPoint PPT presentation

Number of Views:286
Avg rating:3.0/5.0
Slides: 59
Provided by: cao6
Category:

less

Transcript and Presenter's Notes

Title: An Arbitrary LagrangianEulerian Finite Element Formulation for Dynamics and Finite Strain Plasticity


1
An Arbitrary Lagrangian-Eulerian Finite Element
Formulation for Dynamics andFinite Strain
Plasticity Models
  • Gang Cao
  • Dept. of Civil Engineering
  • Oregon State University

2
Outline
  • Basics of Continuum Mechanics
  • Constitutive Model Finite Strain Plasticity
  • Initial Boundary Value Problem
  • Uncoupled ALE Formulation
  • Numerical simulations

3
1. Basics of Continuum Mechanics
is a material body
4
The motion of a material body
5
1. Basics of Continuum Mechanics
Picking out two neighboring configurations, we
get
6
1. Basics of Continuum Mechanics
Reference configuration M is fixed and
independent of any placement of the material body
7
Displacement Field
Physical displacement in Reference configuration
Material displacement
Spatial displacement
Displacement of mesh point m
8
Velocity Fields
Using chain rule
Mesh velocity
Convective velocity
Material velocity
Spatial velocity
9
Acceleration Fields
In reference configuration
Material Acceleration
Spatial Acceleration
Mesh Acceleration
10
General material time derivative
The physical acceleration can also be written as
For any function f(x), the material time
derivative can be written as
Local accel.
convective accel.
11
Deformation gradient
Similarly, we can define
12
Concept of Stress
Cut out a part of the body and denote the
remaining part as and in the material and
the spatial configuration. is
the Cauchy traction vector.
is the First piola-Kirchhoff (or nominal)
traction vector
  • Eulers cut principle

Cauchy stress tensor
First Piola Kirchhoff stress tensor
13
Concept of Stress
Second Piola Kirchhoff stress tensor
Kirchhoff stress tensor
14
2. Constitutive Model Finite Strain Plasticity
Representation of the multiplicative
decomposition of the deformation gradient into
its plastic and elastic contribution
15
Finite Strain Plasticity in Tensor Notation
16
Numerical Implementation
  • Integration of the Flow Rules----Implicit Scheme

17
The Elastic Predictor
The elastic predictor leads to the elastic trial
state
18
The Elastic Predictor
Total Lagrange Formulation
Updated Lagrange Formulation
The Kuhn-Tucker complementary conditions
19
The Elastic Predictor
  • Elastic step

If lt0, then the trial elastic state with
satisfies the Kuhn-Tucker conditions.
Then the trial elastic step is the solution at
time
  • Plastic step

When gt0, it means that is non
admissible and cannot be the solution at time
. This should be corrected by plastic corrector
20
The Plastic Corrector
21
Spectral Decomposition
And define principal elastic logarithmic
stretches by
Substitute these formulas into previous
equations, we get
22
Finite strain plasticity in spectral
Decomposition
23
3. Initial Boundary Value Problem (IBVP)
Problem Definition in the referential
configuration
24
Strong Form of the IBVP
25
Weak Form of the IBVP
26
Finite Element Discretization
27
Finite Element Discretization
  • Spatial velocity

Convective velocity
28
Finite Element Discretization
  • Approximation for the internal variables

29
Finite Element Discretization
30
4. Uncoupled ALE Formulation
----The Operator Split
  • Linear advection equation

Split
Eulerian Equation
Lagrangian Equation
31
The Operator Split
  • By using Taylor-series expansion for variable
    , we get
  • Lagrangian phase

Lagrangian Equation
  • Eulerian phase

Eulerian Equation
Where,
and
32
The Operator Split
  • The features of Smoothing Phase
  • Boundary nodes are required to remain on the
    boundary, since this is the main advantage of the
    ALE formulation compared to the Eulerian one.
    This can be obtained by allowing only a
    tangential movement to the boundary of these
    nodes
  • Mesh distortion is controlled by moving inner
    nodes in an appropriate way

33
Application of Operator Split Technique to the
ALE Formulation
Not the same point any more
Keep the physical motion constant
Material Body and mesh move together
34
Application of Operator Split Technique to the
ALE Formulation
35
Application of Operator Split Technique to the
ALE Formulation
Illustration of the Updated Lagrange Formulation
used in the Lagrangian Phase of the ALE
formulation
36
Flowchart of the Uncoupled ALE formulation
37
The Smoothing Phase
  • Laplacian Based Approach

38
The Smoothing Phase
  • Element Area Based Approach

39
Convective Velocity
after smooth
before smooth
  • Mesh velocity
  • Convective velocity

40
Eulerian Phase----Final solution of the internal
variables
  • Velocities are computed at mesh nodes
  • The stress-related internal variables normally
    lie inside the elements
  • This yields a discontinuous stress field, because
    we need we need compute spatial gradient of these
    internal variables

Two method to compute the derivatives of the
Lagrangian solution of theinternal variable with
respect to time
  • Lax-Wendroff Scheme
  • Godunov-scheme

41
Lax-Wendroff Scheme
We need a smoothed field of spatial gradient of
the internal variable
42
Lax-Wendroff Scheme
classical least squares projection
43
Godunov Scheme
  • Without computing the spatial gradient
  • Directly compute the derivatives of the
    Lagrangian solution of the internal variable with
    respect to time

Define
Conservative form
44
Godunov Scheme ----One-point-quadruatu
re
Assume piecewise constant field of the solution
of the internal variable after the Lagrangian
phase.
Take the weak form
Where is the internal variable component
along the side s of the element under
consideration, stands for the total number
of sides of the element and is the
volume of the element
45
Godunov Scheme ----One-point-quadruatu
re
46
Godunov Scheme ----One-point-quadruatu
re
where
is the flux of convective velocity
47
Godunov Scheme ----multiple-point-quad
ruature
Illustration of the Godunov scheme for
Multiple-point-quadrature
48
5. Numerical Simulations
----Impact of a Circular Bar
Smoothing strategy
Equidistantly distributed in radial direction
49
Impact of a Circular Bar
Non-uniform distribution in radial direction
50
Impact of a Circular Bar
Equidistantly distributed in radial direction
51
Impact of a Circular Bar
  • Theres not much difference between the
    Lagrangian and the ALE formulation
  • The time step in ALE formulation is four times
    larger than one in Lagrangian formulation, which
    means ALE formulation can be much faster than the
    Lagrangian formulation although in every time
    step ALE need extra smooth phase and Eulerian
    phase after the Lagrangian phase

52
Necking of a Circular Bar
For ALE and Lagrangian computation
For the reference solution
53
Smooth Strategy
Equidistantly distributed
Fixed the vertical position
Equidistantly distributed in radial direction
54
Comparison of Spatial Meshes
Large deformation
Uniform distributed
55
Necking of a Circular Bar
constant in horizontal direction
not constant in horizontal direction
56
Conclusion
  • The results from uncoupled ALE formulation are
    reliable
  • The ALE formulation can be much faster than
    Lagrangian formulation because it can use larger
    time step without large element deformation

57
Reference
1 Christian Linder, An Arbitrary
Lagrangian-Eulerian Finite Element Formulation
for Dynamics and Finite Strain Plasticity Models,
Master thesis, University of Stuttgart,
German,2003
58
  • Thank you, everyone!!!
Write a Comment
User Comments (0)
About PowerShow.com