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Effect of blade leading edge thickness on cavitation performance of 80.6 deg helical inducer in hydrogenEffect of blade leading edge thickness on cavitation performance of helical inducer in hydrogen
Document ID
19700021516
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Meng, P. R. (NASA Lewis Research Center Cleveland, OH, United States)
Moore, R. D. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1970
Subject Category
Fluid Mechanics
Report/Patent Number
E-5445
NASA-TN-D-5855
Accession Number
70N30827
Funding Number(s)
CONTRACT_GRANT: 128-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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