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Experimental investigation of a low Reynolds number partial admission single stage supersonic turbinePartial admission performance of single stage supersonic turbine at low Reynolds numbers
Document ID
19710026938
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Goldman, L. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-2382
E-6380
Accession Number
71N36414
Funding Number(s)
PROJECT: RTOP 120-34
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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