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Spin-tunnel investigation of a 1/20 scale model of a modified straight-wing, twin-boom, counter-insurgency airplaneSpin tunnel investigation of 1/20 scale model of modified straight-wing, twin boom, counter insurgency airplane
Document ID
19700031341
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lee, H. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1970
Subject Category
Aircraft
Report/Patent Number
L-7142
NASA-TM-X-2053
Report Number: L-7142
Report Number: NASA-TM-X-2053
Accession Number
70N40657
Funding Number(s)
CONTRACT_GRANT: 126-63-11-32
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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