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Maximum lift-drag-ratio characteristics of rectangular and delta wings at mach 6.9Lift-drag-ratio characteristics of rectangular and delta wings at Mach 6.9
Document ID
19650021975
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Penland, J. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-2925
Report Number: NASA-TN-D-2925
Accession Number
65N31576
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DELTA WING
MACH NUMBER
RECTANGULAR WING

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