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Instantaneous and dynamic analysis of supersonic inlet-engine compatibilityWind tunnel tests for instantaneous and dynamic analysis of effects of time-variant distortions produced in supersonic inlet on J85-GE-13 turbojet engine
Document ID
19710014451
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Burstadt, P. L. (NASA Lewis Research Center Cleveland, OH, United States)
Calogeras, J. E. (NASA Lewis Research Center Cleveland, OH, United States)
Coltrin, R. E. (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-67821
Report Number: NASA-TM-X-67821
Accession Number
71N23927
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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