Film cooling performance evaluation of bi-directional diffusion hole with compound-angle on turbine blade: Study on spanwise width

Author:

Li Bingran,Liu Cunliang,Ye Lin,Ren Ming,Wang Siyi,Liu Song

Publisher

Elsevier BV

Reference46 articles.

1. Effect of hot-streak counts on turbine blade heat load and forcing;He;J. Propul. Power,2007

2. A review of gas turbine effusion cooling studies;Krewinkel;Int. J. Heat Mass Transf.,2013

3. A review of shaped hole turbine film cooling technology;Bunker;Int. J. Heat Mass Transf.,2005

4. Film-cooling effectiveness downstream of a single row of holes with variable density ratio;Sinha;J. Turbomach.,1991

5. Film cooling effectiveness and heat transfer analysis of a hybrid scheme with different outlet configurations;Ghorab;Appl. Therm. Eng.,2014

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