Effects of mainstream cross-flow and wall contouring on film cooling effectiveness of cylindrical-holes embedded in elliptical craters

Author:

Xu Shuai,Pu Jian,Wang Jian-hua,Chen Yun,Wu Wei-long

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference32 articles.

1. Gas turbine film cooling;Bogard;J. Propuls. Power,2012

2. Thermal barrier coated surface modifications for gas turbine film cooling: a review;Krishna Anand;J. Thermal Anal. Calorim.,2021

3. Film cooling of a contoured endwall nozzle vane through fan-shaped holes;Barigozzi;Int. J. Heat Fluid Flow,2010

4. A review of shaped hole turbine film-cooling technology;Bunker;J. Thermophys. Heat Transf.,2005

5. Fric T.F., Campbell R.P., Method for improving the cooling effectiveness of a gaseous coolant stream which flows through a substrate, and related articles of manufacture, U.S. Patent No.6,383,602 (2002-5-7).

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