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strain analysis

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minny

minny

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Nov 1, 2008
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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
 
Yes. You have to ask for it to be output. Check the manual for the appropriate parameters.
 
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