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Large-scale low-speed wind-tunnel tests of a delta winged supersonic transport model to determine aerodynamic effects of forward or reverse thrustLarge scale low speed wind tunnel tests of delta winged supersonic transport model to determine aerodynamic effects of forward and reverse thrust
Document ID
19670022812
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Aoyagi, K. (NASA Ames Research Center Moffett Field, CA, United States)
Tolhurst, W. H. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1964
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-1017
Report Number: NASA-TM-X-1017
Accession Number
67N32141
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC TRANSPORT
THRUST
DELTA WING
WIND TUNNEL MODEL
AERODYNAMIC CHARACTERISTICS

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