Multi-step optimizations of leading edge and downstream film cooling configurations on a high pressure turbine vane

Author:

Jiang Yuting,Wan Xinchao,Magagnato FrancoORCID,Yue Guoqiang,Zheng QunORCID

Funder

National Natural Science Foundation of China

Natural Science Foundation of Heilongjiang Province of China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference23 articles.

1. Numerical investigations of pulsed film cooling on an entire turbine vane;Ke;Appl. Therm. Eng.,2015

2. Gas Turbine Heat Transfer and Cooling Technology;Han,2013

3. Effects of side hole position and blowing ratio on sister hole film cooling performance in a flat plate;Wu;Appl. Therm. Eng.,2016

4. E.R. Turner, M.D. Wilson, L.D. Hylton et al., Analytical and Experimental Evaluation of Surface Heat Transfer Distrubutions with Leading Edge Showerhead Film Cooling, NASA-CR-174827, 1985.

5. An experimental study of turbine vane heat transfer with leading edge and downstream film cooling;Nirmalan;ASME J. Turbomach.,1990

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