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Evaluation with a turbofan engine of air jets as a steady-state inlet flow distortion device Technical memorandumTurbofan engine used for evaluating air jets as steady state inlet flow distortion device
Document ID
19700007983
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Braithwaite, W. M. (NASA Lewis Research Center Cleveland, OH, United States)
Dicus, J. H. (NASA Lewis Research Center Cleveland, OH, United States)
Moss, J. E., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-1955
E-5325
Report Number: NASA-TM-X-1955
Report Number: E-5325
Accession Number
70N17288
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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