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Shock Tube Tests of a Kevlar Sandwich Panel and Comparison with Theory US Army Ballistic Research Laboratory, Aberdeen Proving Ground, MD

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Allison, W. Don, author.
Conference Name:
Aerospace Technology Conference & Exposition (1987-10-05 : Long Beach, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1987
Summary:
Two large identical sandwich panels having face sheets made of Kevlar 49 cloth and epoxy matrix were tested against blast in an eight foot (2.44 m) diameter shock tube. Plastic deformation occurred in both panels. The central displacement and the applied pressure were recorded and used with simple beam theory to calculate the dynamic modulus of elasticity and the dynamic yield strength in compression of the Kevlar composite
Notes:
Vendor supplied data
Publisher Number:
871894
Access Restriction:
Restricted for use by site license

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