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WIND-TUNNEL INVESTIGATION AT SUBSONIC AND SUPERSONIC SPEEDS OF A MODEL OF A TAILLESS FIGHTER AIRPLANE EMPLOYING A LOW-ASPECT-RATIO SWEPT-BACK WING-STABILITY AND CONTROLSubsonic and supersonic wind tunnel study of low aspect ratio sweptback wing tailless fighter aircraft model/stability and control
Document ID
19630003988
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Smith, W. G. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 1, 2013
Publication Date
January 12, 1953
Subject Category
Biosciences
Report/Patent Number
NACA-RM-A52J30
Report Number: NACA-RM-A52J30
Accession Number
63N13864
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY AND CONTROL
TAILLESS AIRCRAFT
SUPERSONIC WIND TUNNEL
LOW ASPECT RATIO WING
WIND TUNNEL
SUBSONIC WIND TUNNEL
SWEPTBACK WING
FIGHTER AIRCRAFT

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