Impact of thermal radiation on turbine blades with film cooling structures

Author:

Li Haiwang,Wang Meng,You Ruquan,Tao Zhi

Funder

National Major Science and Technology Projects of China

Fundamental Research Funds for the Central Universities

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference21 articles.

1. Experimental investigation on the effect of hole diameter on the leading edge region film cooling of a twist turbine blade under rotation conditions;Li;Appl. Therm. Eng.,2021

2. Combined film and impingement cooling of flat plate with reverse cooling hole;Singh;Appl. Therm. Eng.,2022

3. Experimental study on performance verification test of optimized film cooling holes in a linear cascade;Zhang;Appl. Therm. Eng.,2022

4. Effects of an incoming vortex on the film cooling jet;Wang;Int. J. Heat Mass Transf.,2022

5. W. Wang, P. Sun, J. Ren, H. Jiang, Radiative effectiveness on the aero- and thermodynamics in a highly thermally loaded film cooling system, In: Proceedings of the ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. Vancouver, British Columbia, Canada, 2011, Paper No: GT2011-45592, pp. 325-334. 10.1115/GT2011-45592.

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