Week - 10 Hyperelastic Material Models
Modelling a Hyperelastic material from raw data
Hyperelastic material-
these materials have the properties or ability to regain it original shape even after applying large strains, the material may sustain upto 500% of strain.
Aim- to convert the raw material data of hyperelastic material to Keyword properties or ls-dyna mat properties (both Mat-77_O and Mat-77_H)and simulate the model of dogbone specimen to validate the data.
given
engineering stress and engineering strain of material are given data
step 1
obtain the values of all constants in Mat-77_H by giving stress and strain curve as load curve(LCSS) from d3Hsp file
for N=1
C01 and C10 are obtained
for N=2
C01,C10,C11,C22,C20 are obtained
for N=3
C01,C10,C11,C22,C20,C30 are obtained
from d3hsp file true stress and true strain are obtained from which verification are done by converting into e.stress and e stress

then the obtained constants are given as input for all N=1,2,3
the results are as follows and simulated
N=1

the maximum strain is 0.74

the max stress is 1.95 mpa
N=2

the max strain is o.505

the max stress is 1.2 mpa
N=3

the max strain os 0.38

the max stress is 0.8 mpa
the simulation is done results are validated by comparing stress and strains
the data obtained for n2 and n3 are less than n1 because of convergence problems during solving.
the above process is also carried for ogden material constants are obtained
for N=1
Mu1, Alpha 1 are obtained
for N=2
Mu1,Mu-2,alpha 1,alpha 2 are obtained
For N=3
Mu1,Mu-2,alpha 1,alpha 2,Mu-3,alpha 3 are obtained
from d3hsp file the stretch and stress values are obtained and verification is done by comparing values of given
then the obtained constants are given as input for all N=1,2,3

the results are as follows and simulation is done and results are compared and validation is done.
For N=1

the max stress is 1.46 mpa

the max strain is 0.612
for N=2

the max strain is 0.663

the max stress is 1.8 mpa
for N=3

the max stress is 2.3 Mpa

the max strain is 0.65
the simulation is done results are validated by comparing stress and strains
the data obtained for n2 and n3 are less than n1 because of convergence problems during solving.
Conclusion-
The given data is converted into both Mat-77_H and Mat-77_O. the obtained data is verified and validated by simulation values. the values are near to accurate values.hence the project is completed.the excel file is attached for verification.