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Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a V/STOL airplane configuration with a variable-sweep wing and with a skewed wing designStatic longitudinal and lateral aerodynamic characteristics of V/STOL aircraft with variable sweep wing
Document ID
19660013086
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Foster, G. V. (NASA Langley Research Center Hampton, VA, United States)
Morris, O. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1961
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-521
Report Number: NASA-TM-X-521
Accession Number
66N22375
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
V/STOL AIRCRAFT
VARIABLE SWEEP
SWEPT WING
STATIC AERODYNAMIC CHARACTERISTICS

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