how if i want to create a material with only E1, E2, v12 and G12? because in CLT plane element don't consider the direction of Z axial. i used ACP and transform to shell element, but if a change the value of G23, the result won't be the same? but i should be the same. why? can you help me?
Thx for great video sir
It was of much help to me in my project
plz give a video of composite material analysis of a ship rudder
Thank you
Do you have analysis results? Can you also share the article with values?
how if i want to create a material with only E1, E2, v12 and G12? because in CLT plane element don't consider the direction of Z axial. i used ACP and transform to shell element, but if a change the value of G23, the result won't be the same? but i should be the same. why? can you help me?
Is there any tutorial for Metal matrix composites, kindly suggest if any
I am not getting the shell view option beside history view
what to do?
Nyc sir can tell me how to do composite analysis of pressure vessel using 5 layers
Add layers in stack sequence as in 03:18
what happen to me
"An unknown error occurred during solution. Check the Solver Output on the Solution Information object for possible causes."