Effects of turbine blade tip shape on total pressure loss and secondary flow of a linear turbine cascade
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference24 articles.
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2. Bindon, J.P., 1987. Pressure distribution in the tip clearance region of an unshrouded axial turbine as affecting the problem of tip burnout. In: Proc. of International Gas Turbine Conference, Anaheim, California, USA, 87-GT-230.
3. Axial turbine blade tips: function, design, and durability;Bunker;J. Propuls. Power,2006
4. Aerodynamics of tip leakage flows near partial squealer rims in an axial flow turbine stage;Camci;J. Turbomach.,2005
5. Chyu, M.K., Yu, Y., Ding, H., Downs, J.P., Soechting, F.O., 1997. Concavity enhanced heat transfer in an internal cooling passage. In: Presented at the International Gas Turbine and Aeroengine Congress and Exhibition, Orlando, Florida, USA, 97-GT-437.
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