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Analytical investigation of two-dimensional loss characteristics of supersonic turbine stator bladesFlow angle and throat Reynolds number effects on loss characteristics of two dimensional supersonic nozzle
Document ID
19690021982
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Goldman, L. J. (NASA Lewis Research Center Cleveland, OH, United States)
Vanco, M. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1823
Report Number: NASA-TM-X-1823
Accession Number
69N31360
Funding Number(s)
CONTRACT_GRANT: 128-31-32-07-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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