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An integrated approach to the analysis and design of wings and wing-body combinations in supersonic flowNumerical procedure for analyzing and designing wings and wing-body combinations in supersonic flow
Document ID
19660029459
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Carmichael, R. L. (NASA Ames Research Center Moffett Field, CA, United States)
Woodward, F. A. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3685
Accession Number
66N38749
Funding Number(s)
CONTRACT_GRANT: 126-13-02-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC FLOW
NUMERICAL ANALYSIS
WING BODY

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