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Spin-tunnel investigation of a 1/20-scale model of a straight-wing, twin-boom, counter-insurgency airplaneSpin-tunnel investigation of scale model of straight wing, twin boom counter insurgency airplane
Document ID
19690025610
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
August 1, 1969
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-1602
Report Number: NASA-TM-X-1602
Accession Number
69N34988
Funding Number(s)
CONTRACT_GRANT: 737-05-00-02-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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