Accession Number : ADA290642
Title : High Velocity Impact and Penetration of Thick Composite Laminates.
Descriptive Note : Final rept.,
Corporate Author : PURDUE UNIV LAFAYETTE IN SCHOOL OF AERONAUTICS AND ASTRONAUTICS
Personal Author(s) : Sun, C. T.
PDF Url : ADA290642
Report Date : 26 OCT 1994
Pagination or Media Count : 10
Abstract : Ballistic impact of thick-section composites is an extremely complex technical problem. In this research project we have introduced a new approach in using the quasi-static punch curve to describe the mechanics of penetration. Using this punch curve, we are able to capture the mechanical characteristics of penetration and avoid modeling the untractable damage progression in the target during penetration. (MM)
Descriptors : *IMPACT, *LAMINATES, *TERMINAL BALLISTICS, *ARMORED VEHICLES, COMPOSITE MATERIALS, PROJECTILES, HIGH VELOCITY, STIFFNESS, DISPLACEMENT, FIBER REINFORCED COMPOSITES, IMPACT STRENGTH, CRACK PROPAGATION, PENETRATION, GRAPHITE EPOXY COMPOSITES.
Subject Categories : Laminates and Composite Materials
Distribution Statement : APPROVED FOR PUBLIC RELEASE