Heat Transfer for a Turbine Blade With Nonaxisymmetric Endwall Contouring
Author:
Affiliation:
1. Department of Mechanical and Nuclear Engineering, Pennsylvania State University, University Park, PA 16802
2. Pratt & Whitney, 400 Main Street, East Hartford, CT 06108
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4000542/5845457/011019_1.pdf
Reference29 articles.
1. Crossflows in a Turbine Passage;Langston;ASME J. Eng. Power
2. Predictions of Endwall Losses and Secondary Flows in Axial Flow Turbine Cascades;Sharma;ASME J. Turbomach.
3. Turbulent Transport on the Endwall in the Region Between Adjacent Turbine Blades;Goldstein;ASME J. Heat Transfer
4. Effects of Tip Endwall Contouring on the Three-Dimensional Flow Field in an Annular Turbine Nozzle Guide Vane: Part 1—Experimental Investigation;Boletis;ASME J. Eng. Gas Turbines Power
5. Secondary Loss Measurements in a Cascade of Turbine Blades With Meridional Wall Profiling;Morris
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