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Effect of wing leading-edge shape on aerodynamic characteristics of a 67 deg swept wing-body model at Mach 1.50 to 4.63Effect of wing leading-edge shape on aerodynamic characteristics of 67 deg swept wing-body model at Mach 1.50 to 4.63
Document ID
19660028010
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Feryn, M. O. (NASA Langley Research Center Hampton, VA, United States)
Kyle, R. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3634
Accession Number
66N37300
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC SPEED
AERODYNAMIC CHARACTERISTICS
LEADING EDGE
SWEPT WING

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