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Cold-air investigation of a turbine with transpiration-cooled stator blades. 1 - Performance of stator with discrete hole bladingTranspiration coolant ejection effects on stator mass flow and efficiency
Document ID
19700030523
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Prust, H. W., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Schum, H. J. (NASA Lewis Research Center Cleveland, OH, United States)
Szanca, E. M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1970
Subject Category
Aerodynamics
Report/Patent Number
E-5550
NASA-TM-X-2094
Accession Number
70N39839
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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