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Energy-Absorbing Airframes for General AviationConcept for protecting people in lightweight airplane crashes involves redesigning area between interior floor and outer skin of airplane belly to create subfloor strong enough to bear stresses of flight but crush under force of impact. Several concepts evaluated and five selected and designed as lower fuselage sections tested in NASA's crash-testing program. Notched corner concept, Corrugated Beam concept, Foam-Filled Cylinder concept, Corrugated Half Shell concept, and Canted Bulkhead concept. Experimental and analytical results indicate all five concepts perform well; upper floor remains structurally intact whereas crush zone collapses under essentially constant load.
Document ID
19840000111
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Carden, H. D.
(Helicopter Textron, Inc.)
Hayduk, R. J.
(Helicopter Textron, Inc.)
Cronkhite, J.
Berry, V.
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12808
ISSN: 0145-319X
Report Number: LAR-12808
Accession Number
84B10111
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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