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The role of fiber and matrix in crash energy absorption of composite materialsStatic crushing tests were conducted on tube specimens fabricated from graphite/epoxy, Kevlar/epoxy and hybrid combinations of graphite-Kevlar/epoxy to examine the influence the fiber and matrix constitutive properties and laminate architecture have on energy absorption. Fiber and matrix ultimate failure strain were determined to significantly effect energy absorption. The energy absorption capability of high ultimate failure strain materials (AS-6/F185 and AS-6/HST-7) was less than materials having lower ultimate failure strain. Lamina stacking sequence had up to a 300 percent change in energy absorption for the materials tested. Hybridizing with graphite and Kevlar reinforcements resulted in materials with high energy absorption capabilities that have postcrushing integrity.
Document ID
19870026407
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Farley, G. L.
(NASA Langley Research Center; U.S. Army, Aviation Systems Command, Hampton VA, United States)
Bird, R. K.
(NASA Langley Research Center Hampton, VA, United States)
Modlin, J. T.
(Missouri-Rolla, University MO, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Composite Materials
Accession Number
87A13681
Distribution Limits
Public
Copyright
Other

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