strain analysis

[minny]

Hi
I'm running a fea of a composite skin. The composite is a laminated composite with ply in 0,45,-45,90 direction. The skin is modeled with CQUAD.
I've to check the strain.
May I obtain the strain at each ply? Is it available in *.F06 ?

thanks

 

[SWComposites]

Yes. You have to ask for it to be output. Check the manual for the appropriate parameters.