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Large-scale wind-tunnel investigation of the low-speed aerodynamic characteristics of a supersonic transport model having variable- sweep wingsLarge scale wind tunnel investigation of low speed aerodynamic characteristics of supersonic transport model having variable sweep wings
Document ID
19650014225
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Aoyagi, K. (NASA Ames Research Center Moffett Field, CA, United States)
Cook, A. M. (NASA Ames Research Center Moffett Field, CA, United States)
Greif, R. K. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-2824
Report Number: NASA-TN-D-2824
Accession Number
65N23826
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRCRAFT MODEL
WIND TUNNEL STABILITY TEST
LOW SPEED STABILITY
AERODYNAMIC CHARACTERISTICS
VARIABLE SWEEP
SWEPT WING
SUPERSONIC TRANSPORT

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