Affiliation:
1. Grumman Aerospace Corporation Bethpage, New York 11714
Abstract
Using a newly developed boundary layer theory for laminated compos ites, a complete analytical solution is obtained for all the interlaminar shear stresses as well as the normal or "peel" stress of a finite strip in unidirec tional extension. Results obtained by the present analysis are compared to the finite-difference solution of Pipes and Pagano, and to the analytical solution of Puppo and Evensen.
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Cited by
102 articles.
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