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Effects of lee-surface volume addition on longitudinal aerodynamics of a high-lift-drag-ratio wing-body configuration at Mach 6.0Volume addition effects on leeward surface of high lift drag ratio winged body at hypersonic speeds
Document ID
19680008411
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Ashby, G. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Stone, D. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4361
Report Number: NASA-TN-D-4361
Accession Number
68N17880
Funding Number(s)
CONTRACT_GRANT: 124-07-02-57-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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