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Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable-sweep WingsWind tunnel tests of stability and control of variable sweep wing aircraft at Mach 1.97
Document ID
19660022441
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
August 1, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-323
Report Number: NASA-TM-X-323
Accession Number
66N31731
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC STABILITY
SUPERSONIC WIND TUNNEL
VARIABLE SWEEP

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