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Spin-tunnel investigation of a 1/30-scale model of a subsonic attack airplaneSpin and recovery characteristics of 1/30 scale subsonic attack aircraft model determined in wind tunnel tests
Document ID
19690028594
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lee, H. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 5, 2013
Publication Date
August 1, 1969
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-1788
Report Number: NASA-TM-X-1788
Accession Number
69N37976
Funding Number(s)
CONTRACT_GRANT: 737-05-00-01-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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