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Effect of geometric modifications on the maximum lift-drag ratios of slender wing-body configurations at hypersonic speedsGeometric modifications effect on lift-drag ratios of wing body configurations at hypersonic speeds
Document ID
19660010303
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Bertram, M. H. (NASA Langley Research Center Hampton, VA, United States)
Small, W. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3276
Accession Number
66N19592
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING BODY
HYPERSONIC SPEED
LIFT-DRAG RATIO

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