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1.050 Engineering Mechanics

Lecture 22:

Isotropic elasticity

1.050 – Content overview

I. Dimensional analysis

1.

On monsters, mice and mushrooms

2.

Similarity relations: Important engineering tools

II. Stresses and strength

3.

Stresses and equilibrium

4.

Strength models (how to design structures, foundations.. against mechanical failure)

III. Deformation and strain

5.

How strain gages work?

6.

How to measure deformation in a 3D structure/material?

IV. Elasticity

7.

Elasticity model – link stresses and deformation

8.

Variational methods in elasticity

V. How things fail – and how to avoid it

9.

Elastic instabilities

10.

Plasticity (permanent deformation)

11.

Fracture mechanics

Lectures 1-3

Sept.

Lectures 4-15

Sept./Oct.

Lectures 16-19

Oct.

Lectures 20-31

Oct./Nov.

Lectures 32-37

Dec.

1.050 – Content overview

I. Dimensional analysis

II. Stresses and strength

III. Deformation and strain

IV. Elasticity

Lecture 20: Introduction to elasticity (thermodynamics)

Lecture 21: Generalization to 3D continuum elasticity

Lecture 22: Special case: isotropic elasticity

Lecture 23: Applications and examples

V. How things fail – and how to avoid it

Important concepts: Isotropic elasticity

• Isotropic elasticity = elastic properties do not depend on direction

• In terms of the free energy change , this means that the change of the free energy does not depend on the direction of deformation

• Rather, it depends on quantities that are independent on the direction of deformation (i.e., independent of coordinate system)

• Idea: Use invariants of strain tensor to calculate free energy change

– Volume change

– Shape change (shear deformation)

• Note: Invariants are defined as properties of strain tensor that are independent of coordinate system (C.S.)

Important mathematical tools tr

( )

= ε

: 1

= ε

11

+ ε

22

+ ε

33

= d

Ω − d

Ω d 0 d

0

Trace of a tensor

Relates to the chain of volume of REV

Independent of C.S. – trace of a tensor is an invariant

ε =

2

1

(

ε

:

ε T

)

=

1

∑∑

ε

2 i j ij

2

‘Magnitude’ of a tensor (2 nd order norm)

Note: Analogy to the ‘magnitude’ of a tensor is the norm of a first order tensor

(=vector), that is, its length

Overview: Approach

Step 1: Calculate change in volume

ε v

= tr

(

ε

)

= ε

: 1

Step 2: Calculate magnitude of angle change

Define strain deviator tensor = tensor that describes deformation without the volume change ( trace of strain deviator tensor is zero!

)

ε e

ε −

1 tr

3

( )

1 ⎟ d

=

2 e

=

2

2

1

( e : e

T tr

( )

=

)

=

2

ε

11

+ ε

22

1

∑∑

e

2 i j ij

2

+ ε

33

1 (

3

(

3

ε

11

+ ε

22

+ ε

33

))

=

0

Step 3: Define two coefficients to link energy change with deformation

(“spring model”):

Ψ =

1

2

K

ε

2 + v

1

2

G

ε d

2

Shear modulus Bulk modulus

Note

The approach that the free energy under deformation depends only on volume change and overall angle change is not derived from physical principles

Rather, it is an assumption, which is made to ‘model’ the behavior of a solid

( modeling is finding a mathematical representation of a physical phenomenon )

Generally, models must be validated, for instance through experiments

Alternative approach: Calculation of from ‘first principles’ – by explicitly considering the atomistic scale of atomic, molecular etc. interactions

Spring 2008: 1.021J Introduction to Modeling and Simulation (Buehler,

Radovitzky, Marzari) – continuum methods, particle methods, quantum mechanics

Stress-strain relation

Total stress tensor = sum of contribution from volume change and contribution from shape change:

σ = σ + σ v d

σ = v

∂Ψ v

∂ ε

σ = d

∂Ψ d

∂ ε

Next step : Carry out differentiations

Stress-strain relation

Total stress tensor = sum of contribution from volume change and contribution from shape change:

σ = σ + σ v d

σ = v

∂Ψ v

∂ ε

σ d

=

∂Ψ d

∂ ε

1. Calculation of

Ψ v

=

1

K

2

ε v

2

σ v

σ v

=

∂Ψ v

∂ ε

=

∂Ψ v

∂ ε v

:

ε

ε v

=

K

ε v

1

∂Ψ v

∂ ε v

=

K

ε v

∂ ε

∂ ε v

=

(tr(

∂ ε

ε

))

=

(

ε

∂ ε

: 1)

=

1

Stress-strain relation

2. Calculation of

σ d

σ = d

∂ Ψ d

∂ ε

Ψ d

=

1

G

2

ε d

2

=

∂ Ψ d

∂ e

:

∂ e

ε

=

2 Ge :

1

1

3

1

1

=

2 Ge

1

3

( e : 1

)

1

=0

∂Ψ

∂ e d

=

1

2

G

(

2 e : e

T

∂ e

)

=

2 Ge

Note (definition of

ε d

=

2 e

=

2

ε d

):

1

2

( e : e

T

)

∂ e

∂ ε

=

1

1

1

1

3 tr since:

( e

)

=

0 tensor product

Note (definition of e

): e

= ε −

1

3

ε v

1

= ε −

1

3

(

ε

: 1)

1

Complete stress-strain relation

3. Putting it all together:

σ = σ + σ v d

σ =

K

ε v

1

+

2 Ge

=

K

ε v

1

+

2 G

ε −

1

3

ε v

1

⎠ e

= ⎜ ε −

1

3 tr

( )

1

Deviatoric part of the strain tensor

σ =

K

2

3

G

⎟ ε v

1

+

2 G

ε

Reorganized…

Complete stress-strain relation

σ = ⎜

K

2

3

G

ε v

1

+

2 G

ε = ⎜

K

2

3

G

( ε

11

+ ε

22

+ ε

33

)

1

+

2 G

ε

Writing it out in coefficient form:

σ

11

σ

22

σ

33

=

=

=

K

K

K

2

3

2

3

2

3

G

G

G

( ε

( ε

( ε

11

11

11

+

+

+

ε

22

ε

22

ε

22

+

+

+

ε

33

)

+

2 G

ε

11

ε

ε

33

)

+

2 G

ε

33

)

+

2 G

ε

22

33

σ

12

=

2 G

ε

12

σ

23

=

2 G

ε

23

σ

13

=

2 G

ε

13

Complete stress-strain relation

Rewrite by collecting terms multiplying

ε ii

σ

σ

σ

11

22

33

=

=

=

K

+

K

K

4

3

2

3

2

3

G

G

G

ε

ε

ε

11

11

11

+

+

+

K

K

K

+

2

3

4

3

2

3

G

G

G

ε

ε

ε

22

22

22

+

+

+ ⎜⎛

K

K

K

+

2

3

2

3

4

3

G

G

G

ε

ε

ε

33

33

33

… collecting terms multiplying

σ

12

=

2 G

ε

12

ε

12

,

ε

23

,

ε

13

σ

23

=

2 G

ε

23

σ

13

=

2 G

ε

13

(1)

(2)

(3)

Complete stress-strain relation

σ

11

=

K

+

4

3

G

⎟ ε

11

+ ⎜

K

2

3

G

⎟ ε

22

+

K

2

3

G

⎟ ε

33

(1) c

1111

=

K

+

4

G

3 c

1122

=

K

2

G

= c

3

1133

Complete stress-strain relation

σ

22

=

K

2

3

G

⎟ ε

11

+ ⎜ K

+

4

3

G ⎟ ε

22

+

K

2

3

G ⎟ ε

33 (2) c

2211

=

K

2

G

= c

3

2233 c

2222

=

K

+

4

G

3

Complete stress-strain relation

σ

33

= ⎜

K

2

3

G

ε

11

+ ⎜

K

2

3

G

ε

22

+ ⎜⎛

K

+

4

G

⎝ 3 ⎠

ε

33

(3) c

3311

=

K

2

G

= c

3

3322 c

3333

=

K

+

4

G

3

Complete stress-strain relation

σ

12

=

2 G

ε

12

σ

23

=

2 G

ε

23

σ

13

=

2 G

ε

13 c

1212

=

2 G c

2323

=

2 G c

1313

=

2 G

All other c ijkl are zero

Summary: Expression of elasticity tensor

c

1111

= c

2222

= c

3333

=

K

+

4

G

3 c

1122

= c

1133

= c

2233

=

K

2

G

3 c

1212

= c

2323

= c

1313

=

2 G

Examples – numerical values

Concrete

K = 14 GPa G = 10 GPa

Quartz (sand, stone..)

K = 27 GPa G = 26 GPa

Steel

K = 200 GPa G = 140 GPa

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