Film-Cooling Flowfields With Trenched Holes on an Endwall
Author:
Affiliation:
1. Creative Power Solutions USA, Inc., 11010 North Saguaro Boulevard, Fountain Hills, AZ 85268
2. Department of Mechanical and Nuclear Engineering, Pennsylvania University, University Park, PA 16802
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.3068316/5845943/041007_1.pdf
Reference26 articles.
1. Distribution of Film-Cooling Effectiveness on a Turbine Endwall Measured Using Ammonia and Diazo Technique;Friedrichs;ASME J. Turbomach.
2. Aerodynamic Aspects of Endwall Film-Cooling;Friedrichs;ASME J. Turbomach.
3. Bunker, R. S. , 2002, “Film-Cooling Effectiveness Due to Discrete Holes Within a Transverse Surface Slot,” ASME Paper No. GT2002–30178.
4. High-Resolution Film Cooling Effectiveness Measurements of Axial Holes Embedded in a Transverse Trench With Various Trench Configurations;Waye;ASME J. Turbomach.
5. Bump and Trench Modifications to Film-Cooling Holes at the Vane Endwall Junction;Sundaram;ASME J. Turbomach.
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3. Upstream Endwall Film-Cooing in a Vane Cascade with Cylindrical Shape Holes;Journal of Thermophysics and Heat Transfer;2023-07
4. A combined cooling structure consisting of serrated trench and V-shaped surface for film holes: Flow structure and effectiveness improvement;International Journal of Thermal Sciences;2023-07
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