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Performance of an auxiliary inlet ejector nozzle with fixed inlet doors and triple-hinge trailing-edge flapPerformance of auxiliary inlet ejector nozzle with fixed inlet doors and triple-hinge trailing edge flap over subsonic and transonic free stream range for supersonic aircraft
Document ID
19700022736
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Johns, A. L. (NASA Lewis Research Center Cleveland, OH, United States)
Steffen, F. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-2034
E-5497
Report Number: NASA-TM-X-2034
Report Number: E-5497
Accession Number
70N32047
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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