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Longitudinal aerodynamic characteristics at Mach 1.50 to 4.63 of a missile model employing various canards and a trailing edge flap controlWind tunnel static longitudinal stability and control characteristics of cruciform delta winged missile with various horizontal canards and trailing-edge flap control between Mach 1.50 and 4.63
Document ID
19710026939
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Trescot, C. D., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-2367
L-6163
Report Number: NASA-TM-X-2367
Report Number: L-6163
Accession Number
71N36415
Funding Number(s)
PROJECT: RTOP 760-74-01-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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