Volume 1: Turbomachinery 1996
DOI: 10.1115/96-gt-037
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Study of Radial Tip Clearance Effects in a Low-Speed Axial Compressor Rotor

Abstract: A three-dimensional space marching code is used for the numerical modelling of the flow in an isolated axial flow compressor rotor. The rotor is analyzed at four operating points, up to near stall conditions. Numerical results are first validated veisus available experimental data and then further exploited in eider to illuminate flow patterns in the inter-blade region. The tip. leakage impact on the main passage flow and losses level as well as the effect of blade loading on the hub corner stall extent and th… Show more

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