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Crash energy absorbing composite sub-floor structureStatic crushing tests were conducted on four different beam concepts; honeycomb sandwich, sine-wave and two integrally stiffened designs. The sine-wave beams, depending upon specimen geometry, has the highest energy absorption potential of the four concepts evaluated. All beam designs produced a progressive crushing mode similar to tube specimens. The energy absorption capability of sine-wave beam specimens were predictable from results of circular cross section tubes. A comparison of energy absorption capability was made between integrally stiffened beams fabricated from graphite/epoxy, Kevlar-49/epoxy and aluminum. The energy absorption capability of the graphite/epoxy integrally stiffened beams exceeded both the Kevlar-49/epoxy and aluminum integrally stiffened beams. The energy absorption potential of composite structures is between five and ten times that of comparable metallic structure.
Document ID
19860054214
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Farley, G. L.
(NASA Langley Research Center; U.S. Army, Aerostructures Directorate, Hampton VA, United States)
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 86-0944
Accession Number
86A38952
Distribution Limits
Public
Copyright
Other

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