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Development of airframe design technology for crashworthiness.This paper describes the NASA portion of a joint FAA-NASA General Aviation Crashworthiness Program leading to the development of improved crashworthiness design technology. The objectives of the program are to develop analytical technology for predicting crashworthiness of structures, provide design improvements, and perform full-scale crash tests. The analytical techniques which are being developed both in-house and under contract are described, and typical results from these analytical programs are shown. In addition, the full-scale testing facility and test program are discussed.
Document ID
19730049875
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kruszewski, E. T.
Thomson, R. G.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
April 1, 1973
Subject Category
Aircraft
Report/Patent Number
SAE PAPER 730319
Meeting Information
Meeting: Business Aircraft Meeting
Location: Wichita, KS
Start Date: April 3, 1973
End Date: April 6, 1973
Sponsors: Society of Automotive Engineers
Accession Number
73A34677
Distribution Limits
Public
Copyright
Other

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