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Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot locationAerodynamic characteristics of aircraft configuration for low level supersonic attack tested in transonic wind tunnel
Document ID
19650017034
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bielat, R. P. (NASA Langley Research Center Hampton, VA, United States)
Pierpont, P. K. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-429
Report Number: NASA-TM-X-429
Accession Number
65N26635
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL
AERODYNAMIC CHARACTERISTICS
SUPERSONIC STRIKE AIRCRAFT
AIRCRAFT CONFIGURATION

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