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Analytical investigation of the effect of cooling air on two-stage turbine performanceFlow analysis to determine turbine efficiency as function of inlet temperature for two stage turbine
Document ID
19690008060
Document Type
Technical Memorandum (TM)
Authors
Whitney, W. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1969
Subject Category
AERODYNAMICS
Report/Patent Number
NASA-TM-X-1728
Funding Number(s)
CONTRACT_GRANT: 126-15-02-31-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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NameType 19690008060.pdf STI