Influence of spacing of a delta-winglet vortex generator pair on the flow behavior and heat transfer at the internal tip of gas turbine blades

Author:

Zhao Zhiqi,Luo Lei,Qiu Dandan,Wang Songtao,Wang Zhongqi,Sundén BengtORCID

Publisher

Elsevier BV

Subject

General Engineering,Condensed Matter Physics

Reference40 articles.

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2. Heat transfer coefficients on the squealer tip and near squealer tip regions of a gas turbine blade;Kwak;J. Heat Tran.,2003

3. Effects of winglet geometry on the aerodynamic performance of tip leakage flow in a turbine cascade;Zhou;ASME J. Turbomach.,2013

4. Investigations of film-cooling effectiveness on the squealer tip with various film-hole configurations in a linear cascade;Cheng;Int. J. Heat Mass Tran.,2018

5. The augmentation of internal blade tip-cap cooling by arrays of shaped pins;Bunker;ASME J. Turbomach.,2008

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