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Computer program describing turbine aerodynamic requirements, approximate external blade geometries, and coolant flow requirements for a two stage axial flow turbineComputer program to generate turbine aerodynamic requirements, approximate external blade geometries, and coolant flow requirements for two stage axial flow turbine
Document ID
19710013092
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Evans, D. G. (NASA Lewis Research Center Cleveland, OH, United States)
Furgalus, K. A. (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
April 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-2229
E-6014
Report Number: NASA-TM-X-2229
Report Number: E-6014
Accession Number
71N22568
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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