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Favorable interference effects on maximum lift-drag ratios of half-cone delta-wing configurations at mach 6.86Investigation of half-cone delta wing configurations under laminar boundary layer conditions at Mach 6.86 to determine favorable interference effects on maximum lift-drag ratio
Document ID
19650021976
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Fetterman, D. E. (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-2942
Report Number: NASA-TN-D-2942
Accession Number
65N31577
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DELTA WING
INTERFERENCE DRAG
LAMINAR BOUNDARY LAYER
HYPERSONIC SPEED
HALF-CONE
LIFT-DRAG RATIO

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