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AERODYNAMIC CHARACTERISTICS OF SEVERAL FLAT-BOTTOM CONFIGURATIONS AT MACH 3.0 AND 3.5Aerodynamic characteristics of flat-bottom wing- body combinations at mach 3.0 and 3.5
Document ID
19630003037
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Dryer, M. (NASA Lewis Research Center Cleveland, OH, United States)
Luidens, R. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1959
Subject Category
Aircraft
Report/Patent Number
NASA-MEMO-1-2-59E
Report Number: NASA-MEMO-1-2-59E
Accession Number
63N12913
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC SPEED
BODY-WING COMBINATION
WING
AERODYNAMIC CHARACTERISTICS
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