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Ditching Investigation of a Dynamic Model of a HU2K-1 HelicopterVarious configurations and approach conditions were investigated in order to determine the ditching behavior and the best ditching procedure. When ditchings were made without the float bags, the model rolled over on its side; when ditchings were made with the float bags inflated, the model remained upright. Late-flare and early-flare ditchings gave the same general behavior. Slight damage to the bottom surface of the scale-strength fuselage resulted for all test conditions.
Document ID
19980227860
Acquisition Source
Headquarters
Document Type
Technical Memorandum (TM)
Authors
Thompson, William C.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1961
Subject Category
Air Transportation And Safety
Report/Patent Number
N-AM-42
NASA-TM-SX-626
NASA-AD-3142
Report Number: N-AM-42
Report Number: NASA-TM-SX-626
Report Number: NASA-AD-3142
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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