Unsteady effects of vortex interaction on tip leakage vortex breakdown and its loss mechanism
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference32 articles.
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2. Blade loading effects on axial turbine tip leakage vortex dynamic and loss;Huang,2012
3. Control of tip leakage vortex breakdown by tip injection in unshrouded turbines;Gao;J. Propuls. Power,2014
4. Comparison of turbine tip leakage flow for flat tip and squealer tip geometries at high-speed conditions;Key;J. Turbomach.,2006
5. The reduction of over tip leakage loss in unshrouded axial turbines using winglet and squealers;Schabowski,2007
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