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Inlet-engine-nozzle wind tunnel test techniquesWind tunnel tests of supersonic propulsion inlet, engine and exhaust nozzles
Document ID
19710019470
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bowditch, D. N. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-67870
E-6416
Report Number: NASA-TM-X-67870
Report Number: E-6416
Accession Number
71N28946
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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