Experimental study of combined influences of wall curvature and compound angle on film cooling effectiveness of a fan-shaped film-hole
Author:
Publisher
Elsevier BV
Subject
Condensed Matter Physics,General Chemical Engineering,Atomic and Molecular Physics, and Optics
Reference20 articles.
1. Review of platform cooling technology for high pressure turbine blades;Wright,2014
2. Experimental study of free-stream turbulence intensity effect on overall cooling performances and solid thermal deformations of vane laminated end-walls with various internal pin-fin configurations;Pu;Appl. Therm. Eng.,2020
3. Conjugate heat transfer measurements and predictions of a blade endwall with a thermal barrier coating;Mensch;J. Turbomach.,2014
4. Experimental flow field investigations of a film cooling hole featuring an orifice;Zheng;Appl. Therm. Eng.,2014
5. A review of shaped hole turbine film-cooling technology;Bunker;J. Thermophys. Heat Transf.,2005
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