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xxx Markus J. Buehler Deformation of Ductile Materials (contd) Fracture of brittle materials Lecture 5 From nano to macro: Introduction to atomistic modeling techniques IAP 2007

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Page 1: Deformation of Ductile Materials (contxxx Fracture ... - MIT OpenCourseWare · Lennard-Jones potential Schematic Displacement in 112 direction in 10-10 M&F V&C O&J BAM Consequence:

xxx

Markus J. Buehler

Deformation of Ductile Materials (cont’d)Fracture of brittle materials

Lecture 5

From nano to macro: Introduction to atomistic modeling techniques

IAP 2007

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© 2007 Markus J. Buehler, CEE/MIT

Outline

1. Introduction to Mechanics of MaterialsBasic concepts of mechanics, stress and strain, deformation, strength and fractureMonday Jan 8, 09-10:30am

2. Introduction to Classical Molecular DynamicsIntroduction into the molecular dynamics simulation; numerical techniquesTuesday Jan 9, 09-10:30am

3. Mechanics of Ductile MaterialsDislocations; crystal structures; deformation of metals Tuesday Jan 16, 09-10:30am

4. The Cauchy-Born ruleCalculation of elastic properties of atomic latticesFriday Jan 19, 09-10:30am

5. Dynamic Fracture of Brittle MaterialsNonlinear elasticity in dynamic fracture, geometric confinement, interfacesWednesday Jan 17, 09-10:30am

6. Mechanics of biological materialsMonday Jan. 22, 09-10:30am

7. Introduction to The Problem SetAtomistic modeling of fracture of a nanocrystal of copper. Wednesday Jan 22, 09-10:30am

8. Size Effects in Deformation of MaterialsSize effects in deformation of materials: Is smaller stronger?Friday Jan 26, 09-10:30am

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© 2007 Markus J. Buehler, CEE/MIT

Outline and content (Lecture 5)

Topic: Fracture mechanisms in ductile and brittle materials.

Examples: Large-scale simulation of a copper nanocrystal – analysis of dislocation mechanisms

Material covered: Metallic bonding, EAM potentials, energy approach to elasticity, Cauchy-Borne rule; basics in fracture mechanics –prediction of dislocation nucleation and crack extension

Important lesson: Dislocation as fundamental carrier of plasticity, driving force for fracture processes, competition between ductile and brittle processes

Historical perspective: Origin of Griffith’s fracture theory

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Ductile versus brittle materials

BRITTLE DUCTILE

Glass Polymers Ice...

Shear load

Copper, Gold

© 2006 Markus J. Buehler, CEE/MIT

Figure by MIT OCW.

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© 2007 Markus J. Buehler, CEE/MIT

Derivation stress field around crack tip

See lecture notes

σxy

σrθσrr

σθθ

σxx

σyy

r

x

y

θ

Figure by MIT OCW.

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© 2007 Markus J. Buehler, CEE/MIT

EQ eq.

Compat. cond.

Airy stress function: Ansatz

Asymptotic stress field

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© 2007 Markus J. Buehler, CEE/MIT

Stress field around a (static) crack

Hoop or opening stress

Maximum principal stress

0.2σ xx

0.4

0.6v/cr = 0

0

0 50θ

100 150

σ XY

v/cr = 0

0-0.2

-0.1

0.1

0.2

0

50θ

100 150

0.2σ yy

0.4

0.6

v/cr = 0

0

0 50θ

100 150

Continuum theoryMD modeling

σ θ

0.2

0.4

0.6

v/cr = 0

0

0 50θ

100 150σ 1

0.5

1

1.5v/cr = 0

00 50

θ100 150

Figure by MIT OCW.

Figure by MIT OCW.Figure by MIT OCW.

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Ductile materials are governed by the motion of dislocations: Introduction

Figure by MIT OCW.

Dislocations are the discrete entities that carry plastic (permanent) deformation; measured by “Burgers vector”

http://www.people.virginia.edu/~lz2n/mse209/Chapter7.pdf © 2006 Markus J. Buehler, CEE/MIT

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© 2007 Markus J. Buehler, CEE/MIT

Partial dislocations

In FCC, dislocations with Burgers vector [110] split up into two“partial dislocations” with Burgers vector 1/6[112]

http://www.tf.uni-kiel.de/matwis/amat/def_en/kap_5/backbone/r5_4_2.html

Metals with low SFE and materials under geometric confinement often have large stacking faultsImage removed due to copyright restrictions.

See the first image on this page:

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© 2007 Markus J. Buehler, CEE/MIT

Partial dislocations

Stacking fault: Long range atomic order distorted HCP vs. FCC

B

b3 b2 b1

B B B B BA A A A A

d

Stacking Fault

Glide plane

Burgers vectorof complete dislocation

Burgers vectors of partial dislocations

B B B B BA A A A A A

Figure by MIT OCW.

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© 2007 Markus J. Buehler, CEE/MIT

Dislocation nucleation from a crack tip

• Critical load for cracking• What happens when the load becomes large?• How to analyze the complex data?• Limitations of modeling…

Figure by MIT OCW.

Copper

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© 2007 Markus J. Buehler, CEE/MIT

Atomistic details of dislocation nucleation

• Dislocation nucleation from a traction-free grain boundary in an ultra thin copper film

• Atomistic results depict mechanism of nucleation of partial dislocation

Figure removed for copyright reasons.Source: Figure 16 in Buehler, Markus J., Balk, John, Arzt, Eduard, and Gao, Huajian. "Constrained Grain Boundary Diffusion in Thin Copper Films." Chapter 13 in Handbook of Theoretical and Computational Nanotechnology. Edited by Michael Rieth and Wolfram Schommers. Stevenson Ranch, CA: American Scientific Publishers, 2006.

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© 2007 Markus J. Buehler, CEE/MIT

Chemical bonding in metals“metallic bonding”

Bonding between atoms with low electronegativity 1,2 or 3 valence electrons, therefore there are many vacancies in valence shell.When electron clouds overlap, electrons can move into electron cloud of adjoining atoms.Each atom becomes surrounded by a number of others in a three-dimensional lattice, where valence electrons move freely from one valence shell to another.Delocalized valence electrons moving between nuclei generate a binding force to hold the atoms together

Thus:Electron gas model Mostly non-directional bonding, but the bond strength indeed depends on the environment of an atom, precisely the electron density imposed by other atoms

positive ions in a sea of electrons

+ + + + + +

+ + + + + +

+ + + + + +

+

Electron (q=-1)

Ion core (q=+N)+ +

+ +

+ +

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© 2007 Markus J. Buehler, CEE/MIT

Properties of metals

Reflection of light by electron gasLustrous

Tightly packed FCC, BCC, HCPHigh density

Physical/atomic reasonProperty

Glide (and climb) of dislocationsMany metals are ductile

Delocalized electrons (flow in and out)Good electrical conductors

Vibration transport via delocalized electrons (+phonons)Good conductors of heat

Strong forces between ion core and delocalized electronsHigh melting temperature

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© 2007 Markus J. Buehler, CEE/MIT

Why pair potentials fail…

In pair potentials, the strength of each bond is dependent only on the distance between the two atoms involved: The positions of all the other atoms are not relevant (works well e.g. for Ar where no electrons are available for bonding and atoms are attracted with each other only through the weak van der Waals forces)However: QM tells that the strength of the bond between two atoms is affected by the environment (other atoms in the proximity)As a site becomes more crowded, the bond strength will generally decrease as a result of Pauli repulsion between electrons. The modeling of many important physical and chemical properties depends crucially on the ability of the potential to "adapt to the environment"

Can not reproduce surface relaxation (change in electron density)

http://www.fisica.uniud.it/~ercolessi/forcematching.html

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© 2007 Markus J. Buehler, CEE/MIT

Modeling attempts: Pair potential

First attempts using pair potentials∑

=

=neighNj

iji r..1

)(ϕφ

⎥⎥

⎢⎢

⎟⎟⎠

⎞⎜⎜⎝

⎛−⎟

⎟⎠

⎞⎜⎜⎝

⎛=

612

4)(ijij

ij rrr σσεϕ

Morse

Lennard-Jones 12:6

Good for noble gas Ar(FCC in 3D)

)( ijrϕ

6 5

j=1

2 3

4

cutr

i

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© 2007 Markus J. Buehler, CEE/MIT

Numerical implementation of neighbor search:Reduction of N2 problem to N problem

• Need nested loop to search for neighbors of atom i: Computational disaster

• Concept: Divide into computational cells (“bins”, “containers”, etc.)

• Cell radius R>Rcut (cutoff)

• Search for neighbors within cell atom belongs to and neighboring cells (8+1 in 2D)

• Most classical MD potentials/force fields have finite range interactions

• Other approaches: Neighbor lists

• Bin re-distribution only necessary every 20..30 integration steps (parameter)

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© 2007 Markus J. Buehler, CEE/MIT

Modeling attempts: Multi-body potential

Multi-body potential depend on more than pairs of atoms, but instead also on the environment of each atomImportant for metals due to existence of “electron gas”

)()(21

..1i

Njiji Fr

neigh

ρϕφ += ∑=

First proposed by Finnis, Sinclair, Daw, Baskes et al. (1980s)

Pair potential energy

Embedding energy

as a function of electron density

iρ Electron density at atom Ibased on a pair potential:

∑=

=neighNj

iji r..1

)(πρ

new

6 5

j=1

2

i

3

4

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© 2007 Markus J. Buehler, CEE/MIT

Numerical implementation of multi-body EAM potential

Requires two loops over atoms within each cell

Loop 1:

(i) Pair contributions (derivatives and potential)

(ii) Calculate electron density

Loop 2:

(iii) Calculate embedding function and derivatives

Due to additional (i) calculation of electron density and (ii) embedding contribution EAM potentials are 2-3 times slower than pure pair potentials

O Or

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Stacking fault energy: LJ potential vs. EAM potential

/(

)

0 0 1

( )[ ] ( m)

0.01

0.02

0.03

0.04

0.05

0.06

0.07

Ener

gyat

om e

V

0.5 1.5

us

sf

Lennard-Jones potential

SchematicDisplacement in 112 direction in 10-10

M&F V&C O&J BAM

Consequence: Only partial dislocations expected

Figure by MIT OCW. After Buehler and Gao, "Ultra large scale atomistic simulations of dynamic fracture," 2006.

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© 2007 Markus J. Buehler, CEE/MIT

Separation of partial dislocations

Width of stacking fault

⎟⎠⎞

⎜⎝⎛

−−

−−

=νβν

νν

πγμ

2)2cos(21

12

8

2

sfe

br

Approaches infinity for 0→sfγ

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© 2007 Markus J. Buehler, CEE/MIT

Deformation of metals: Example

http://www.kuleuven.ac.be/bwk/materials/Teaching/master/wg02/l0310.htm

Image removed for copyright reasons.See: Fig. 4 at http://www.kuleuven.ac.be/bwk/materials/Teaching/master/wg02/l0310.htm.

Image removed for copyright reasons.See: Fig. 6 at http://www.kuleuven.ac.be/bwk/materials/Teaching/master/wg02/l0310.htm.

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© 2007 Markus J. Buehler, CEE/MIT

Strengthening mechanisms

????

Figure by MIT OCW.

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© 2007 Markus J. Buehler, CEE/MIT

Strengthening mechanisms

Remember: Theoretical shear strength of materials is not reached due to the existence of dislocationsBy hindering the motion or the possibility to create dislocations, the material becomes stronger, approaching the theoretical strengthMechanisms:

Grain boundary strengthening Images removed due to copyright restrictions.

Grain size reduction

Introduction of foreign atoms that create strain field (solid-solution strengthening)

Introduction of particles that pin/hinder dislocation motion

http://www.people.virginia.edu/~lz2n/mse209/Chapter7.pdf

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© 2007 Markus J. Buehler, CEE/MIT

Need: Large system size to generate large number of dislocations

Micrometer range of dislocation-dislocation interactionsThus: Need crystal with 100..200 nm side length – 1E9 atoms

Image removed for copyright reasons.See: Fig. 4 at http://www.kuleuven.ac.be/bwk/materials/Teaching/master/wg02/l0310.htm.

Figure by MIT OCW. After Buehler et al, 2005.

(1 1 0)

[1 1 0]

[1 1 0] Crack faces

Mode 1 tensile loading

Y

Z

X

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© 2007 Markus J. Buehler, CEE/MIT

Simulation details

1,000,000,000 atom

Lennard-Jones ductile “model material”

φ

r

Genericfeatures of atomicbonding: „repulsion vs. attraction“

Analysis of a one-billion atom simulation of work-hardening

(1 1 0)

[1 1 0]

[1 1 0] Crack faces

Mode 1 tensile loading

Y

Z

X

[ ]

[ ]

y = [ ]

[ ][ ]

[ ]

001

Crack Direction 1 1 0

100

z = 001x = 110

010

Figure by MIT OCW. After Buehler et al, 2005.Figure by MIT OCW. After Buehler et al, 2005.

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Increase in computing powerClassical molecular dynamics

2 5

6

8

9

/L ( ) ( )

( )

10 atoms 10 atoms 10 atoms

10 atoms

10 atoms

1011 atoms

"Teraflop"

1965 1975 1985 1995 2005 2012 Year

Computer power BlueGene USA 70 TFLOP NASA Ames USA 50 TFLOP Earth Simulator Japan 40 TFLOP LINUX Clusters

IBM Almaden Spark

"Gigaflop"

"Petaflop" computers

Figure by MIT OCW.

(Buehler et al., to appear 2006)

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Parallel Molecular Dynamics

Figure by MIT OCW.

(after Schiotz)

Concept:

Divide the workload

No (immediate) long range interaction (only via dynamics)

• Each CPU is responsible for part of the problem

• Atoms can move into other CPUs (migration)

• Need to know topology or the geometric environment on other CPUs (green region)

• 1,000,000,000 particles on 1,000 CPUs: Only 1,000,000 atoms/CPU

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© 2007 Markus J. Buehler, CEE/MIT

Implementation of parallelization

Shared memory systems (all CPUs “see” same memory)OpenMP (easy to implement, allows incremental parallelization)POSIX threads

Distributed memory systemsMPI (=Message Passing Interface)Most widely accepted and used, very portable, but need to parallelize whole code at once

Parallelization can be very tedious and time-consuming and may distract from solving the actual problem; debugging difficult

Challenges: Load balancing, different platforms, input/output, compilers and libraries, modifications and updates to codes, “think parallel” as manager

Strategy for your own code: Find similar code and implement your own problem

http://nf.apac.edu.au/training/MPIProg/slides/index.html, http://www.openmp.org/, http://www.eecs.umich.edu/~qstout/parallel.html

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© 2007 Markus J. Buehler, CEE/MIT

Bridging length scales by direct numerical simulation (DNS)

Understand the behavior of complex many-particle systems, without imposing constraints or boundary conditions

Discover new physical phenomena, e.g. collective events that involve a large number of particles

Caution:Need to make sure that model produces useful results, i.e. includes new scientific content and discoveriesPictures may be pretty, but what do we learn?

Why is large-scale modeling useful?

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© 2007 Markus J. Buehler, CEE/MIT

Increase in computing power: Parallelization

Modeling of mechanical behavior of materials is highly demanding and requires models with millions and billions of atoms

200570,000,000,000

particles70 TFLOP computers

20107,000,000,000,000 particles

1,000 TFLOP computers

0.3 µm

1.2 µm

5 µm20001,000,000,000

particles10 TFLOP computers

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© 2007 Markus J. Buehler, CEE/MIT

Lattice around dislocation

Atoms with higher energy than bulk are highlighted

Centrosymmetry method

partial dislocation

Stacking fault

[121]

[111]

b

Analysis of glide plane and Burgers vector

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© 2007 Markus J. Buehler, CEE/MIT

Hardening mechanismscreation of sessile structure1. Dislocation cutting processes: Intersection of dislocations leads to generation of trails of point defects (trails of partial point defects, vacancy tubes and interstitials): when two screw dislocations intersect, each acquires a jog with a direction andlength equal to the Burgers vector of the other dislocation. Upon intersection, the dislocations cannot glide conservatively sinceeach jog has a sessile edge segment.- Energy required to create point defects- Therefore: Pinning of dislocations – dragging force:

Different kinds of point defects

Images removed due tocopyright restrictions.

0 0 0 0 0 0 0 0 -

* 0 0 0 0 0 0 0 0 o o o o o o o 8

1 0 0 0 ~ 0 ~ - o o o o * a I o o o O t

0 0 0 0 ~ 0 0 0 0 o * o * ~ ~ o ~ ~ b

o o o o a o-o-o'~' 0 0 0 1 W W O O O O O Q ~ O O C ~ D

0 0 0 0 ~ ~ 0 0 0 0 0 0 0 0 0 0 o o o o ~ 0 0 0 0 o o o o ~ O o O ~ O ~ Trail of O O O , * O ~ 0 ~ 0 ~ ~ * 0 * 0 * ~ ~ 0 ~ 0 ~ Trail of Partial 0~0,0,' o ~ o ~ o ~ ~ ~ ~ ~ vacancy Tubes a 0 , o o o Interstitials

oOo",~o~bOO~oO,"OOo Point Defects a 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

O O m m & o e D O 00 0 0

Reduced Dragging Force (20% of vacancy tube)

Figure by MIT OCW.

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© 2007 Markus J. Buehler, CEE/MIT

Hardening mechanismscreation of sessile structure

1/3 vacancy defect, volume a03/12 (vacancy: a0

3/4)

1

1

2

2b

b

bb

Reaction of Two Partials

1

2

b

SF

b

Reaction of One Partial w/ SF

1 2

SF

b

(a)(b)Figure by MIT OCW. Figure by MIT OCW.

Figure by MIT OCW.

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© 2007 Markus J. Buehler, CEE/MIT

Hardening mechanismscreation of sessile structure

Sessile segmentPinning

Figure by MIT OCW.

x

Vacancies

Figure removed for copyright reasons. See Fig. 4 in Buehler, M. et al. "The dynamical complexity of work-hardening: a large-scale molecular dynamics

Glide plane for screw

b

b

Glide Plane for Jog

Sessile Segment Pinning

Figure by MIT OCW.

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© 2007 Markus J. Buehler, CEE/MIT

The plots show how two dislocations (denoted by ‘‘1’’and ‘‘2’’) from opposite cracksintersect and create reaction products. When a second reaction takes place at dislocation ‘‘2’’ involving a third dislocation, thedislocation motion is severely hindered which is seen in the bowing out of the dislocations. Many of such reactions occur during thesimulation causing the generation of a complex defect network.

Hardening mechanismscreation of sessile structure

Images removed due to copyright restrictions.

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© 2007 Markus J. Buehler, CEE/MIT

2. Cross-slip

Activation of secondary slip systems by cross-slip and Frank-Read mechanisms: At later stages of the simulation

• After activation of secondary slip systems: More dislocation reactions (e.g. cutting processes).

• “Rediscovered” Fleischer’s mechanism of cross-slip of partials that was proposed 1959

Hardening mechanismscreation of sessile structure

Images removed due to copyright restrictions.

b xz

(111)

(111)[101]

w a

b

c

d

B

D

C

A

y

Figure by MIT OCW.

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© 2007 Markus J. Buehler, CEE/MIT

Observation of cross-slip

• At a critical dislocation density, secondary slip systems are activated

• This enables for additional plasticity to occur, but also further contributes to work-hardening as the dislocation density increases making it more difficult for dislocations to move

Images removed due to copyright restrictions.

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© 2007 Markus J. Buehler, CEE/MIT

Hardening mechanismscreation of sessile structure

3. Formation of Lomer-Cottrell locks

• Formation of sessile Lomer-Cottrell locks, with its typical shape of a straight sessile arm connected to two partial dislocations

• Sessile junctions provide a severe burden for further dislocation glide

Images removed due to copyright restrictions.

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© 2007 Markus J. Buehler, CEE/MIT

Final sessile structure

The characteristic structure of the network:

All sessile defects (both trails of partial and complete point defects) as well as sessile dislocations are straight lines that lie on the edges of Thompson’s tetrahedron (at intersections of stacking fault planes)

Consists of…:Vacancy tubes, interstitials, partial dislocations, and sessile dislocations

Images removed due to copyright restrictions.

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© 2007 Markus J. Buehler, CEE/MIT

Final sessile structure

Image removed due to copyright restrictions.See:1. Buehler, M. J., et al. "The dynamical complexity of work-hardening: a large scale molecular dynamics situation." Acta Mechanica Sinica 21, no. 2 (2005): 103-111.

2. Buehler, M. J., et al. "Atomic plasticity: description and analysis of a one-billion atom simulation of ductile materials failure." Computer Methods in Applied Mechanics and Engineering 193, no. 48-51 (2004): 5257-5282.

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Case study: Cracking of a copper crystal…

• Critical load for cracking• What happens when the load becomes large?• How to analyze the complex data?• Limitations of modeling…

Copper

Figure by MIT OCW.

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© 2007 Markus J. Buehler, CEE/MIT

Dislocation nucleation and fracture condition

Ductile or brittle?

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Energy approach to elasticity

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© 2007 Markus J. Buehler, CEE/MIT

Energy approach to elasticity

1st law of TD

2nd lawApplied force

Change in entropy is always greater or equal than the entropy supplied in form of heat; difference is due to internal dissipation

Dissipation rate

External work rate

Dissipation rate after consider 1st law of TD:

or

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© 2007 Markus J. Buehler, CEE/MIT

Energy approach to elasticity

Elastic deformation:

Assume only internal energy change

Expand equation dU/dt = dU/dx dx/dt

Therefore:

With strain energy density:

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© 2007 Markus J. Buehler, CEE/MIT

Cauchy-Born rule

Idea: Express elastic energy (strain energy density) for a atomistic representative volume element as a function of macroscopic applied strain

DΩ: Mapping function, e.g.

Impose macroscopic deformation gradient on atomistic volume element, then calculate atomic stress – this corresponds to the macroscopic stressStrictly valid only far away from defects in periodic lattice (homogeneous deformation, perfect lattice, amorphous solid-average)

Allows direct link of potential to macroscopic continuum elasticity

U(l) a function of deformation gradient

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1D example: Cauchy-Born rule

Impose homogeneous strain field on 1D string of atomsThen get from thatklijklij c εσ =

))1((1)(1)( 000

rDr

rDr

⋅+⋅

=⋅

=Φ εφφε

r0

Dr ⋅0 Atomic volume

Strain energy densityfunction

F1 F2

1 32

r23r21

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© 2007 Markus J. Buehler, CEE/MIT

Hexagonal lattice

r2

[010]

[100]

y

x

r2 r2

r2

r1r1

r2

r2 r2

r2

r1r1

Figure by MIT OCW.

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Cauchy-Born rule: Hexagonal lattice

Small strains:(Eij are Green-Lagrangian straincomponents from hyperelasticity)

ijijE ε→

Eij

Eij

Λ1

3

1

l3

l2

l1

3Λ2

Θ

Figure by MIT OCW.

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© 2007 Markus J. Buehler, CEE/MIT

Cauchy-Born rule: Stress and elasticity coefficients

Small strains: ijijS σ→

ijklijkl cC →

Small deformations (1st order elastic terms):

This expression is obtained by expanding the potential energy(potential) up to second order terms

( )222'' )(32383

xyyxyyyyxxxx εεεεεεφ ++++=Φ

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Example: Triangular lattice, LJ potential

ε=1σ=1

12:6 LJ potential

r2

[010]

[100]

y

x

r2 r2

r2

r1r1

r2

r2 r2

r2

r1r1

Figure by MIT OCW.

5

4

3

2

1

0 0

00

5

4

3

2

1

0 0

� �

00

[ ] (x) S [ ] (y)

0.1 0.2

0.1 0.2

0.1 0.2

20

40

60

80

Strain xx

Stre

ss

Stre

ss

Strain xx

0.1 0.2

20

40

60

80

Strain yy

Strain yy

Tangent modulus Exx

Strain in 100 -direction train in 010 -direction

Tangent modulus Eyy

LJ Solid Harmonic Solid Poisson ratio LJ solid

Figure by MIT OCW.

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© 2007 Markus J. Buehler, CEE/MIT

Example: Triangular lattice, harmonic potential

00

σ xx,

σyy

, and

νx,

νy

1

2

3

4

0.02 0.04Strain

Stress vs. Strain and Poisson Ratio

0.06 0.08

Stress σxxPoisson ratio νx

Poisson ratio νy

Stress σyy

025

E x, E

y 30

35

40

45

50

0.02 0.04Strain

Tangent Modulus

0.06 0.08

ExEy

Elastic properties of the triangular lattice with harmonic interactions, stress versus strain (left) and tangent moduli Ex and Ey (right). The stress state is uniaxial tension, that is the stress in the direction orthogonal to the loading is relaxed and zero.

Figure by MIT OCW.