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Erosion in radial inflow turbines. Volume 3: Trajectories of erosive particles in radial inflow turbinesThe theoretical trajectories that erosive particles follow in the gas flow fields of a typical radial inflow turbine were investigated. A discussion of the theoretical trajectories that the particles follow in the scroll, in the nozzles, in the vortex between the nozzles and the rotor, and in the rotor passages is included. The results are presented in terms of the characteristic length, a similarity parameter which relates the particles that follow the same trajectory in equivalent flow fields. For Vol, 1, see N74-19395.
Document ID
19750002015
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Clevenger, W. B., Jr.
(Cincinnati Univ. OH, United States)
Tabakoff, W.
(Cincinnati Univ. OH, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1974
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-134700
Report Number: NASA-CR-134700
Accession Number
75N10087
Funding Number(s)
CONTRACT_GRANT: NGR-36-004-055
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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