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Longitudinal aerodynamic characteristics at Mach numbers from 0.50 to 1.19 of a supersonic transport model with a modified M wingLongitudinal aerodynamic characteristics at Mach numbers 0.50 to 1.19 of supersonic transport model with modified M wing
Document ID
19670017971
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ray, E. J. (NASA Langley Research Center Hampton, VA, United States)
Taylor, R. T. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-1386
Accession Number
67N27300
Funding Number(s)
CONTRACT_GRANT: 720-01-00-03-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
M WING
SUPERSONIC TRANSPORT
AIRCRAFT MODEL

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