Winglet geometry effects on tip leakage loss over the plane tip in a turbine cascade
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials
Link
http://link.springer.com/content/pdf/10.1007/s12206-018-0318-2.pdf
Reference49 articles.
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3. R. S. Bunker, J. C. Bailey and A. A. Ameri, Heat transfer and flow on the first-stage blade tip of a power generation gas turbine: part 1-Experimental results, ASME Journal of Turbomachinery, 122 (2000) 263–271.
4. S. W. Lee, H. S. Moon and S. E. Lee, Tip gap height effects on flow structure and heat/mass transfer over plane tip of a high-turning turbine rotor blade, International Journal of Heat and Fluid Flow, 30 (2009) 198–210.
5. Q. Zhang and L. He, Overtip choking and its implications on turbine-tip aerodynamic performance, Journal of Propulsion and Power, 27 (2011) 1008–1014.
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