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Investigation of the aerodynamic characteristics of a hypersonic transport model at Mach numbers to 6Wind tunnel investigation of hypersonic transport model aerodynamic characteristics at Mach numbers to 6 - graphs
Document ID
19710013651
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Ellison, J. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1971
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-6191
L-7478
Report Number: NASA-TN-D-6191
Report Number: L-7478
Accession Number
71N23127
Funding Number(s)
CONTRACT_GRANT: 722-01-10-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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