1
Common hyperelastic
models
2
N
el
2i1
i i
N i
1 i
1 0 i 2
1
J 1
D 3 1
I C
J , I ,
I
Polynomials of the first invariant
Initial shear modulus
0 2C
10Initial compressibility modulus
1 0
2
k D
3
Particular case 1: Neo-Hookean behaviour (N=1)
el
2 11 10 2
1
J 1
D 3 1
I C
J , I ,
I
N
el
2i1
i i
N i
1 i
1 0 i 2
1
J 1
D 3 1
I C
J , I ,
I
Polynomials of the first invariant
4
5
In other words, the material law is not material-frame indifferent
6
7
8
9
10
11
12
el
i Ni i
N i
i
i
J
I D C
J I
I
21 1
1 0 2
1
0
1 1
3 ,
,
Particular case 2: Yeoh behaviour (N=3)
el
ii i
i
i
i
J
I D C
J I
I
23
1 3
1
1 0 2
1
0
1 1
3 ,
,
Forms depending only of the first invariant
polynomials
The usual form of strain energy E I
1, I
2, J
ARRUDA-BOYCE
el
2 el 5
1 i
i i 2 1
i 2 m
i 2
1
0
ln J
2 1 J
D 3 1
C I J
, I , I
673750
; 519 7050
; 19 1050
; 11 20
; 1 2 1
5 4
3 2
1 C C C C
C
Model with 8 chains
Statistical mechanics Gaussian chains
0
k D2
0
Forms depending only of the first invariant
The usual form of strain energy E I
1, I
2, J
sinh
ln n n
Nk chain
0
and 3 3
I1 1 chain
chain
13
14
21 2
01 1
10 2
1
0
1 1
3 3
,
,
J
elI D C
I C
J I
I
Particular case: N=1 MOONEY-RIVLIN
10 01
0
2 C C
1 0
2 k D
Initial shear modulus
Initial compressibility modulus
Forms depending only of the two invariant
polynomials
The usual form of strain energy E I
1, I
2, J
15
OGDEN
el
iN
i i
N
i i
i J
J D I
I i i i 2
1 1
3 2
2 1 2
1
0 1 1
2 3 ,
,
3 2
1
, ,
Principal stretches
i J
31
i
N
i
i 1
0
1 0
2 k D
It is the best model if we have experimental data for numerous tests in different directions
Rivlin Mooney
; 2
; 2
; 2
N 1 2
Hookean Neo
; 2
; 1
N 1
Forms written with the principal stretches
The usual form of strain energy E I
1, I
2, J
Prévisions de l'essai biaxial
0 5 10 15 20 25 30
0,0 0,5 1,0 1,5 2,0 2,5 3,0 3,5 4,0 4,5
Déformation nominale Contrainte nominale (MPa)
Expérience Neo hooke Mooney-Rivlin
Nominal stress (MPa)
Identification of parameters from all the data Prediction of the planar tensile test
16
Stretch λ=L/L0
1 2 3 4 5 6 7
Prevision de l'essai de traction plane
0 5 10 15 20 25
0,0 0,5 1,0 1,5 2,0 2,5 3,0 3,5 4,0 4,5
déformation nominale
contrainte nominale (MPa)
Expérience Ogden N=1 Ogden N=2 Ogden N=3
Engineering stress (MPa)
Identification of parameters from all the data Prediction of the biaxial tensile test
17
Stretch λ=L/L0
1 2 3 4 5 6 7
Prevision de l'essai de traction plane
0 5 10 15 20 25
0,0 0,5 1,0 1,5 2,0 2,5 3,0 3,5 4,0 4,5
déformation nominale contrainte nominale (MPa)
Expérience Yeoh
Arruda-Boyce Van der waals
Engineering stress (MPa)
Identification of parameters from all the data Prediction of the biaxial tensile test
18
Stretch λ=L/L0
1 2 3 4 5 6 7
19
20
21
22
23
24