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Preliminary investigation of performance of a wedge nozzle applicable to a supersonic cruise aircraftPerformance characteristics of wedge nozzle for supersonic cruise aircraft
Document ID
19710008276
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jeracki, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Johns, A. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
E-5894
NASA-TM-X-2169
Report Number: E-5894
Report Number: NASA-TM-X-2169
Accession Number
71N17751
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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