Affiliation:
1. U. S. Air Force Materials Laboratory Wright-Patterson Air Force Base Dayton, Ohio 45433 USA
Abstract
This report presents a procedure to design laminated composite panels subjected to bending loads and in plane loads. The procedure takes advantage of the directionality of the mechanical properties of the composite material using the laminated plates theory.
Subject
Materials Chemistry,Polymers and Plastics,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Cited by
28 articles.
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