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Unstart and stall interactions between a turbojet engine and an axisymmetric inlet with 60-percent internal-area contractionEffects of turbojet engine unstart on engine operation and characteristics of stall propagation through compressor and inlet system
Document ID
19710008663
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)
Choby, D. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-2192
E-5923
Report Number: NASA-TM-X-2192
Report Number: E-5923
Accession Number
71N18138
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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