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Light airplane crash tests at impact velocities of 13 and 27 m/secTwo similar general aviation airplanes were crash tested at the Langley impact dynamics research facility at velocities of 13 and 27 m/sec. Other flight parameters were held constant. The facility, instrumentation, tests specimens, and test method are briefly described. Structural damage and accelerometer data are discussed.
Document ID
19780002091
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Alfaro-Bou, E. (NASA Langley Research Center Hampton, VA, United States)
Vaughan, V. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1977
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA-TP-1042
L-11426
Report Number: NASA-TP-1042
Report Number: L-11426
Accession Number
78N10034
Funding Number(s)
PROJECT: RTOP 505-02-13-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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