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Stability and control characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with outboard wing panels swept back 75 degStability and control of variable sweep wing configuration with outboard wing panels swept back 75 degrees at Mach 2.01
Document ID
19650003085
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Foster, G. V. (NASA Langley Research Center Hampton, VA, United States)
Spearman, M. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-32
Accession Number
65N12686
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SWEPT WING
MACH NUMBER

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