Databor
New member
- Jun 3, 2012
- 6
Hello, I´m performing dynamic buckling analysis in a composite shell. I´m using Nastran SOL129, but I´m facing some difficulties in the analysis. I have enabled large displacements in order to appreciate the buckling. I get perfectly the buckling shape, so it works pretty well in that way, but I´m not able to recover ply stresses or failure indices. Time ago I heard that was not possible to recover these stresses in a non linear transient analysis of composites. Bearing this in mind, I have used the PSHELL+MAT2 equivalent anisotropic elements in order to get the stress tensor of these elements (just for have some information of stresses). As I supposed, displacements are exactly the same than using PCOMP+MAT8, but I´m neither able of recovering the stress tensor.
Therefor it seems that in a nonlinear transient analysis of a model built in anisotropic elements you are not able to recover any kind of stresses. I´ve been trying to solve this issue several days and I´m becoming crazy. I´ve read almost all commands in the Quick Reference Guide, and I´ve done a lot of test without positive results.
So I´m looking to a solution (some command or parameter that I can have overlooked) or someone that tells me that this simply not possible. If it´s not possible, I would also like to know where can I find that issue in order to refer it in my report.
Thank you very much
Therefor it seems that in a nonlinear transient analysis of a model built in anisotropic elements you are not able to recover any kind of stresses. I´ve been trying to solve this issue several days and I´m becoming crazy. I´ve read almost all commands in the Quick Reference Guide, and I´ve done a lot of test without positive results.
So I´m looking to a solution (some command or parameter that I can have overlooked) or someone that tells me that this simply not possible. If it´s not possible, I would also like to know where can I find that issue in order to refer it in my report.
Thank you very much