Vortex shedding mechanisms in relation to tip clearance flows

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dc.contributor.author R. I. Lewis en_US
dc.date.accessioned 2014-10-21T15:51:37Z
dc.date.available 2014-10-21T15:51:37Z
dc.date.issued 1979 en_US
dc.identifier.other ARC/R&M-3829 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3112
dc.description.abstract This paper outlines the importance of tip leakage flows in axial fans as a source of loss and relates the dimensionless loss analytically to a range of dimensionless parameters by application of a jet loss theory due to Rains. Improved vortex shedding models are also presented. From these models theor- etical predictions of lift coefficient reduction are compared with published experimental data for isolated rectangular plates, with experimental tests for a single aerofoil adjacent to a wall with an on-coming boundary layer and correlations due to Lakshminarayana. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title Vortex shedding mechanisms in relation to tip clearance flows en_US


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