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Wind-tunnel investigation of the flow field beneath the fuselage of the X-15 airplane at Mach numbers from 4 to 8Wind tunnel study of flow field beneath X-15 aircraft fuselage at supersonic to hypersonic speeds
Document ID
19680001679
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Montoya, E. 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
November 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-1469
Report Number: NASA-TM-X-1469
Accession Number
68N11147
Funding Number(s)
CONTRACT_GRANT: 729-00-00-01-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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