Effects of Squealer Geometry of Turbine Blade Tip on the Tip-Leakage Flow and Loss

Author:

Zeng Fei,Zhang Weihao,Wang Yufan,Cao Xia,Zou Zhengping

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference36 articles.

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2. Yang H.K., Zhang W.H., Zou Z.P., et al., The development and applications of a loading distribution based tip leakage loss model for unshrouded gas turbines. Journal of Turbomachinery, 2020, 142(7): 1–29.

3. Yang H.K., Zhang W.H., Zou Z.P., Effects of loading distribution on turbine tip leakage losses. Journal of Engineering Thermophysics, 2020, 41(01): 113–121. (in Chinese)

4. Dey D., Camci C., Aerodynamic tip desensitization of an axial turbine rotor using tip platform extensions. ASME Turbo Expo 2001: power for land, sea, and air, New Orleans, United States of America, 2001, V001T03A069.

5. Zhou C., Hodson H., Tibbott I., et al., Effects of winglet geometry on the aerodynamic performance of tip leakage flow in a turbine cascade. Journal of Turbomachinery, 2013, 135(5): 051009.

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