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Investigation of aerodynamic characteristics at high subsonic speeds of two supersonic- cruise airplane configurations having tail surfaces outboard of the wing tipsSubsonic stability and control characteristics of two outboard-tail supersonic-cruise airplane configurations
Document ID
19650003196
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Fournier, P. G. (NASA Langley Research Center Hampton, VA, United States)
Sleeman, W. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-293
Report Number: NASA-TM-X-293
Accession Number
65N12797
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY AND CONTROL
SUBSONIC SPEED
AIRCRAFT CONFIGURATION
SUPERSONIC AIRCRAFT

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