Affiliation:
1. Aerophysics Laboratory, The Aerospace Corporation, El Segundo, Calif.
Abstract
Experimental results are presented for the linear elastic dynamic response of periodically laminated composites. A shock tube-capacitive transducer technique is used to determine the rear surface velocity history of three laminated samples that have different lamination angles and are subjected to a step pressure loading. Viscosity effects are discussed, and comparisons are made with predictions based on previous theoretical work.
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Cited by
6 articles.
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