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Maximum lift-drag ratios of delta-wing-half- cone combinations at a mach number of 20 in heliumMaximum lift-drag ratios of delta wing half-cone combinations in hypersonic helium wind tunnel to determine interference lift
Document ID
19650013005
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Johnston, P. J. (NASA Langley Research Center Hampton, VA, United States)
Snyder, C. D. (NASA Langley Research Center Hampton, VA, United States)
Witcofski, R. D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-2762
Report Number: NASA-TN-D-2762
Accession Number
65N22606
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DELTA WING
INTERFERENCE LIFT
LIFT-DRAG RATIO
HYPERSONIC WIND TUNNEL
HALF-CONE

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