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Erosion in radial inflow turbines. Volume 2: Balance of centrifugal and radial drag forces on erosive particlesThe particle motion in two-dimensional free and forced inward flowing vortices is considered. A particle in such a flow field experiences a balance between the aerodynamic drag forces that tend to drive erosive particles toward the axis, and centrifugal forces that prevent these particles from traveling toward the axis. Results predict that certain sizes of particles will achieve a stable orbit about the turbine axis in the inward flowing free vortex. In this condition, the radial drag force is equal to the centrifugal force. The sizes of particles that will achieve a stable orbit is shown to be related to the gas flow velocity diagram at a particular radius. A second analysis yields a description of particle sizes that will experience a centrifugal force that is greater than the radial component of the aerodynamic drag force for a more general type of particle motion.
Document ID
19740022125
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
April 1, 1974
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-134616
Report Number: NASA-CR-134616
Accession Number
74N30238
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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