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Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87Aerodynamic characteristics of swept wing configuration with progressive series of leading and trailing edge modifications
Document ID
19660017752
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jernell, L. S. (NASA Langley Research Center Hampton, VA, United States)
Mc Kinney, R. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1065
Report Number: NASA-TM-X-1065
Accession Number
66N27042
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
WING PLANFORM
WIND TUNNEL MODEL
SWEPTBACK WING

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