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Stability and control characteristics at low subsonic speeds of an airplane configuration having two types of variable-sweep wingsStatic stability and control at low subsonic speeds of supersonic aircraft with variable sweep wings
Document ID
19660024029
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Spencer, B., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1960
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-303
Accession Number
66N33319
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VARIABLE SWEEP
SUPERSONIC AIRCRAFT
SWEPT WING
SUBSONIC SPEED
STATIC STABILITY AND CONTROL

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