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Flow-field investigations on the X-15 airplane and model up to hypersonic speedsFlow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraft
Document ID
19680025701
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Mc Lain, L. J. (NASA Flight Research Center Edwards, CA, United States)
Palitz, M. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4813
Report Number: NASA-TN-D-4813
Accession Number
68N35173
Funding Number(s)
CONTRACT_GRANT: 719-01-00-03-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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