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Subsonic aerodynamic characteristics of an airplane configuration utilizing a variable- sweep wing having a free-floating apexSubsonic longitudinal characteristics of variable sweep aircraft utilizing free floating wing apex for alleviation of longitudinal stability and supersonic performance problems
Document ID
19660025706
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hammond, A. D. (NASA Langley Research Center Hampton, VA, United States)
Polhamus, E. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1126
Report Number: NASA-TM-X-1126
Accession Number
66N34996
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING
SUBSONIC WIND TUNNEL
VARIABLE SWEEP
ATTACK AIRCRAFT
LONGITUDINAL STABILITY

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