cthen
2007-10-21, 11:20
Dear Dr. Bergstrom & all,
I am working with abaqus using the ogden material model and am determining material constants using an own routine. I would like to implement the Drucker stability check into this routine but the output I get for the stability limits does not correspond to what CAE puts out. For uniaxial loading e.g., I tried to check the stiffnes matrix given in the theory manual Abaq. Version 6.5., Sec. 4.6.2, Ogden form, for positive definitness by varrying lamda_1 in steps of delta_lamda1=0.01 in certain limits and checking if the equations employing D11, D22, D12 and D21 are satisfied. For varification purposes, I did assume an imaginary parameter set (mu_1, alpha_1) and assuming N=1. When checking this parameter set in CAE for Drucker stability, I get different stability ranges for nominal strain then given in my output. Can you tell me what I am doing wrong? Do you possibly have any examplarily routine (c, c++, or any other language) that does the stability check which I possibly could use for orientation? Do you have any suggestions on how to approach the stability check?
Thank you so very much for your help in advance!!! I would be very thankful for any advice regarding my problem!
Kind Regards,
Christophe Then
I am working with abaqus using the ogden material model and am determining material constants using an own routine. I would like to implement the Drucker stability check into this routine but the output I get for the stability limits does not correspond to what CAE puts out. For uniaxial loading e.g., I tried to check the stiffnes matrix given in the theory manual Abaq. Version 6.5., Sec. 4.6.2, Ogden form, for positive definitness by varrying lamda_1 in steps of delta_lamda1=0.01 in certain limits and checking if the equations employing D11, D22, D12 and D21 are satisfied. For varification purposes, I did assume an imaginary parameter set (mu_1, alpha_1) and assuming N=1. When checking this parameter set in CAE for Drucker stability, I get different stability ranges for nominal strain then given in my output. Can you tell me what I am doing wrong? Do you possibly have any examplarily routine (c, c++, or any other language) that does the stability check which I possibly could use for orientation? Do you have any suggestions on how to approach the stability check?
Thank you so very much for your help in advance!!! I would be very thankful for any advice regarding my problem!
Kind Regards,
Christophe Then