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Investigation of a twisted cambered wing with a 75 deg swept leading edge at mach 3 and reynolds numbers to 39 x 106Wing planforms with highly swept subsonic leading edges at Mach 3
Document ID
19650026230
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Moore, J. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3031
Report Number: NASA-TN-D-3031
Accession Number
65N35831
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SWEPTBACK WING
SUBSONIC AIRCRAFT

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