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Sandia is a multiprogram laboratory operated by Sandia Corporation, a Lockheed Martin Company,
for the United States Department of Energy under contract DE-AC04-94AL85000.
Stewart Silling
Multiphysics Simulation Technologies Department
Sandia National Laboratories
Albuquerque, New Mexico, USA
Seminar given at
University of Texas, San Antonio
February 16, 2012
SAND2012-1141C
Multiscale Modeling of Fracture with
Peridynamics
frame 2
First: a puzzle
• Consider a 1D lattice with linear elastic force interactions.
– No transverse loads.
– Prescribed axial displacements at ends.
– The equilibrium displacement field contains transverse deflection as shown.
• What’s going on? – What sort of material would do this?
– Is this even legit mechanically?
Deformed
Undeformed
frame 3
Outline
• Peridynamics basics
• Coarse graining
• Multiscale fracture
frame 4
Purpose of peridynamics
• To unify the mechanics of continuous and discontinuous media within a single,
consistent set of equations.
Continuous body Continuous body
with a defect Discrete particles
• Why do this?
• Avoid coupling dissimilar mathematical systems (A to C).
• Model complex fracture patterns.
• Communicate across length scales.
frame 5
Why this is important
• Cracks:
• Standard approaches implement a fracture model after numerical
discretization.
• Particles:
• Standard approaches require a separate coupling method to relate
particles to continuum.
Complex crack path in a composite
frame 6
Peridynamics basics:
Horizon and family
frame 7
Peridynamics basics:
Bonds and bond forces
frame 8
Peridynamics basics:
Material modeling
frame 9
Kinematics:
Deformation state
frame 10
Material modeling:
Bonds and states
frame 11
Peridynamic vs. standard equations
Kinematics
Constitutive model
Linear momentum
balance
Angular momentum
balance
Peridynamic theory Standard theory Relation
Elasticity
frame 12
Any material model in the classical theory
can be used in peridynamics…
• Example: Large-deformation, strain-hardening, rate-dependent material model.
– Material model implementation by John Foster.
0% strain 100% strain
Necking of a bar under tension
Taylor impact test
Test
Emu
frame 13
…and there are peridynamic materials that
cannot be represented in the standard theory
• Examples
• Bond-pair materials: resist angles changes between opposite bonds.
• Discrete particles: any multibody potential can be represented with peridynamic states.
Multibody potential
Bond-pair
frame 14
Convergence of peridynamics
to the standard theory
In this sense, the standard theory is a subset of peridynamics.
frame 15
How damage and fracture are modeled
Bond elongation
Bond force density Bond breakage
frame 16
Bond breakage forms cracks “autonomously”
Broken bond
Crack path
• When a bond breaks, its load is shifted to its neighbors, leading to progressive failure.
frame 17
Energy balance for an advancing crack
There is also a version of the J-integral that applies in this theory.
Crack
Bond elongation
frame 18
EMU (and LAMMPS) numerical method
• Integral is replaced by a finite sum: resulting method is meshless and Lagrangian.
Method is also available in Sierra (D. Littlewood)
Discretized model in the
reference configuration
• Looks a lot like MD!
• LAMMPS implementation by M. Parks & P. Seleson
frame 19
Predicted crack growth direction depends
continuously on loading direction
• Plate with a pre-existing defect is subjected to
prescribed boundary velocities.
• These BC correspond to mostly Mode-I loading with a
little Mode-II.
Contours of vertical displacement Contours of damage
frame 20
Effect of rotating the grid
in the “mostly Mode-I” problem
Damage Damage, rotated grid
Damage Displacement
Network of identical bonds in many
directions allows cracks to grow in
any direction.
Original grid direction
30deg
Rotated grid direction
frame 21
Fragmentation example:
Same problem with 4 different grid spacings
Dx = 3.33 mm
Dx = 2.00 mm
Dx = 1.43 mm
Dx = 1.00 mm
Brittle ring with
initial radial velocity
frame 22
Dynamic fracture in a hard steel plate
• Dynamic fracture in maraging steel (Kalthoff & Winkler, 1988)
• Mode-II loading at notch tips results in mode-I cracks at 70deg angle.
• 3D EMU model reproduces the crack angle.
EMU*
Experiment
S. A. Silling, Dynamic fracture modeling with a meshfree peridynamic code, in Computational Fluid and Solid Mechanics 2003, K.J. Bathe, ed., Elsevier, pp. 641-644.
frame 23
Example of long-range forces:
Nanofiber network
Nanofiber membrane (F. Bobaru, Univ. of Nebraska)
Nanofiber interactions due to van der Waals forces
frame 24
Peridynamic dislocation model
Example: Dislocation segment in a square with free edges
100 x 100 EMU grid
frame 25
Coarse-graining:
Reducing the degrees of freedom
• Start with a detailed description (level 0).
• Choose a coarsened subset (level 1).
• Model the system using only the coarsened DOFs…
• Forces on the coarsened DOFs depend only on their own displacements.
• These forces should be the same as you would get from the full detailed model.
• After coarsening, the level 0 DOFs no longer are modeled explicitly.
Small-scale MD model
Blue: Level 0
Red: Level 1
Even cats find this interesting
frame 26
Linearized peridynamics
SS, Linearized theory of peridynamic states, J. Elast. (2010)
frame 27
Coarse-graining:
Reduce the number of degrees of freedom
frame 28
Each level’s displacements are determined
by the next higher level
frame 29
Each level has the same mathematical structure
frame 30
Refinement
frame 31
Example: Coarse graining
of an elastic block (answer to puzzle)
Level 0
Level 1
Level 2
• A homogeneous, isotropic rectangle is
stretched from its lower corners.
• Problem is modeled at three levels:
• Level 0 (purple)
• Level 1 (green)
• Level 2 (red)
• Displacements and forces on bc nodes
agree between all three calculations.
Curvature in level 2 results from tensor
nature of the micromoduli.
frame 32
Level 0 composite model
Fiber (red)
Matrix (purple)
2D fiber-reinforced composite: fibers are much stiffer than the matrix.
Stiff bond
Soft bond
frame 33
3 levels of coarsening
0
2
1
3
frame 34
Coarsened composite micromodulus
Level 0 Level 1
Level 2 Level 3
frame 35
Composite bar stretch: displacements
Level 0 Level 1
Level 2 Level 3
frame 36
Level 0 composite model with defect
Fiber (red)
Matrix (purple)
Crack (green)
frame 37
Composite bar with defect:
displacements
Level 0 Level 1
Level 2 Level 3
frame 38
Coarse grained model of Brazilian test
(static crack)
Level 0: 6646 nodes
Level 6357: 289 nodes
Coarsen
Solve on small grid
Refine if needed
Solve on large grid
Load = 5.455
Load = 5.432 Load = 5.441
Almost identical displacements
frame 39
Issues with this coarse graining method
Level 0 Level 1
• Similar to static condensation.
• The number of bonds connected to each node grows with each coarsening level.
• Large memory requirements.
• Experience shows:
• Can be used for coarse-graining relatively small regions or subregions.
• Not suitable for large-scale material mechanics modeling
frame 40
Multiscale approach for growing cracks:
Multiple horizons
Each successive level has a larger
length scale (horizon). Crack process zone
The details of damage evolution
are always modeled at level 0.
frame 41
Multiscale approach for growing cracks:
Concurrent solution strategy
Crack
Level n
Level 2
Level 1
Level 0:
Within distance d of ongoing damage
Level 0
Level 1
Level 2
Level n
Time
Refin
e
Coa
rsen
Solve (fine)
Solve (coarse) R
efin
e
Coa
rsen
Concurrent solution strategy Level 0 region follows the crack tip
• Refinement:
• Level 1 acts as a boundary condition on level 0.
• Coarsening:
• Level 0 supplies material properties (e.g., damage) to higher levels.
frame 42
Crack growth in a brittle plate
Level 2
Level 1 Level 0
Damage process zone
Initial damage
v v
Crack
frame 43
Brittle crack growth:
Bond strain near crack tip
Colors show the largest strain among all bonds connected to each node.
frame 44
Brittle crack growth:
Damage progression and velocity
Damage process zone
v1 velocity
frame 45
Brittle crack under shear loading
Bond strain Damage process zone
frame 46
Crack growth in a heterogeneous medium
• Crack grows between randomly placed hard inclusions.
frame 47
Dynamic brittle crack:
Branching
frame 48
Fracture due to indentation
frame 49
Discussion
• Coarse graining method*:
• Exact but expensive.
• Linear only.
• No adjustable parameters.
• Two-way coupling (coarsening + refinement): consistent multiscale method.
• Multiscale damage method:
• Non-linear, dynamic.
• Low memory requirements.
• Small time step applied only in level 0.
• With big computers, appears to offer the potential to model the details of
heterogeneous material failure at all physically relevant length scales.
*SS, A coasening method for linear peridynamics, Int. J. Multiscale Computational Engineering (2011).
frame 50
Extra slides
frame 51
Nonlocality as a result of homogenization
• Homogenization, neglecting the natural length scales of a system, often doesn’t give good answers.
Indentor Real
Homogenized, local Stress
Claim: Nonlocality is an essential feature of a realistic homogenized model of a heterogeneous material.
frame 52
Proposed experimental method for measuring the peridynamic horizon
• Measure how much a step wave spreads as it goes through a sample.
• Fit the horizon in a 1D peridynamic model to match the observed spread.
Time
Free surface velocity
Peridynamic 1D
Visar
Spread
Projectile Sample
Visar
Laser
Local model would predict zero spread.
frame 53
Material modeling: Composites
frame 54
Splitting and fracture mode change in composites
• Distribution of fiber directions between plies strongly influences the way cracks grow.
Typical crack growth in a notched laminate
(photo courtesy Boeing) EMU simulations for different layups
frame 55
Polycrystals: Mesoscale model*
• Vary the failure stretch of interface bonds relative to that of bonds within a grain.
• Define the interface strength coefficient by
Large favors trans-granular fracture.
*
*
g
i
s
sβ
= 1 = 4 = 0.25
• What is the effect of grain boundaries on the fracture of a polycrystal?
Bond strain
Bond force
*is
*gs
Bond within a grain
Interface bond
* Work by F. Bobaru & students
frame 56
Dynamic fracture in PMMA: Damage features
Microbranching
Mirror-mist-hackle transition*
* J. Fineberg & M. Marder, Physics Reports 313 (1999) 1-108
EMU crack surfaces EMU damage
Smooth
Initial defect
Microcracks
Surface roughness
frame 57
Dynamic fracture in PMMA: Crack tip velocity
• Crack velocity increases to a critical value, then oscillates.
Time (ms)
Cra
ck tip
ve
locity (
m/s
)
EMU Experiment*
* J. Fineberg & M. Marder, Physics Reports 313 (1999) 1-108