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Performance and stall limits of an afterburner-equipped turbofan engine with and without inlet flow distortionPerformance and stall limits of afterburner-type turbofan engine with and without inlet flow distortion
Document ID
19700014942
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Abdelwahab, M. (NASA Lewis Research Center Cleveland, OH, United States)
Braithwaite, W. M. (NASA Lewis Research Center Cleveland, OH, United States)
Werner, R. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
E-5352
NASA-TM-X-1947
Report Number: E-5352
Report Number: NASA-TM-X-1947
Accession Number
70N24247
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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