Author:
MAHMOOD GAZI,Shote Adeola,Huyssen Barbara
Reference40 articles.
1. Influence of hole shape on the performance of a turbine vane endwall film-cooling scheme;W Colban;International Journal of Heat and Fluid Flow,2007
2. A Comparison of Cylindrical and Fan-Shaped Film-Cooling Holes on a Vane Endwall at Low and High Freestream Turbulence Levels;W Colban;Journal of Turbomachinery,2008
3. End-Wall Film Cooling Through Fan-Shaped Holes With Different Area Ratios;G Barigozzi;Journal of Turbomachinery,2007
4. Turbine vane endwall film cooling from mid-chord or downstream rows and upstream coolant injection;N Wang;International Journal of Heat and Mass Transfer,2019
5. Improving turbine endwall cooling uniformity by controlling nearwall secondary flows;M Thomas;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering Part G,2016