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Erosion in radial inflow turbines. Volume 4: Erosion rates on internal surfacesAn analytic study of the rate at which material is removed by ingested dust impinging on the internal surfaces of a typical radial inflow turbine is presented. Results show that there are several regions which experience very severe erosion loss, and other regions that experience moderate levels of erosion loss: (1) the greatest amount of material loss occurs on the trailing edges of the nozzle blades where very high velocity, moderate angle impacts occur. The tip regions of ductile materials are also subjected to serious levels of erosion loss; (2) moderate amounts of erosion occur near the end of the scroll and on a few of the nozzle blades near this location. Results are presented in the form of surface contours that exist on the scroll and blade surfaces after continuous particulate ingestion with time.
Document ID
19750009610
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
January 1, 1975
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-134677
Report Number: NASA-CR-134677
Accession Number
75N17682
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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