Endwall Film-Cooling in a Filleted Vane Cascade with Discrete Slots and Holes Upstream

Author:

MAHMOOD GAZI,Shote Adeola,Huyssen Barbara

Publisher

Elsevier BV

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

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