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The aerodynamic characteristics of several thick delta wings at Mach numbers to 6 and angles of attack 50 degAerodynamic characteristics of thick delta wings at subsonic to supersonic speeds and angles of attack to 50 deg
Document ID
19660024050
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mc Devitt, J. B. (NASA Ames Research Center Moffett Field, CA, United States)
Rakich, J. V. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-162
Report Number: NASA-TM-X-162
Accession Number
66N33340
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DELTA WING
HYPERSONIC SPEED
AERODYNAMIC CHARACTERISTICS
SUBSONIC SPEED
ANGLE OF ATTACK

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