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Aerodynamic Damping and Oscillatory Stability in Pitch and Yaw of a Variable-Sweep Supersonic Transport Configuration at Mach Numbers from 0.40 to 1.80Pitch and yaw characteristics of supersonic transport aircraft with variable sweep wings at various Mach numbers
Document ID
19710007940
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kilgore, R. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1971
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-2164
L-7429
Report Number: NASA-TM-X-2164
Report Number: L-7429
Accession Number
71N17415
Funding Number(s)
CONTRACT_GRANT: 126-13-10-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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