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Experimental investigation of the effects of pulse pressure distortions imposed on the inlet of a turbofan enginePulse pressure distortion effects imposed on inlet of turbofan engine
Document ID
19700001716
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Wenzel, L. M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1969
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-1928
Accession Number
70N11020
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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