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Quiescent-air performance of a truncated turbojet plug nozzle with shroud and plug base flows from a common sourcePerformance characteristics of truncated, conical plug nozzle with cylindrical outer shroud
Document ID
19690018462
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Johns, A. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1969
Subject Category
Physics, Solid-State
Report/Patent Number
NASA-TM-X-1807
Report Number: NASA-TM-X-1807
Accession Number
69N27840
Funding Number(s)
CONTRACT_GRANT: 126-15-02-10-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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