Shock Tube Tests of a Kevlar Sandwich Panel and Comparison with Theory

871894

10/01/1987

Event
Aerospace Technology Conference and Exposition
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/871894
Pages
20
Citation
Allison, W., "Shock Tube Tests of a Kevlar Sandwich Panel and Comparison with Theory," SAE Technical Paper 871894, 1987, https://doi.org/10.4271/871894.
Additional Details
Publisher
Published
Oct 1, 1987
Product Code
871894
Content Type
Technical Paper
Language
English