Bearing-Bypass Basics

[jpaero]

I have been trying develop some intuition when it comes to bearing-bypass interaction in composites. I would like to see a comparison of bearing+bypass stress distribution for metals vs that for laminates. Just to make it simpler for understanding, I was hoping to see the plots if the laminate had only 0deg plies, another laminate with only 90deg plies and yet another with +-45deg.

Would you know any sources?

I posted this in the aerospace forum but then thought that this forum might be more apt.

 

[SWComposites]

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