Experimental and Computational Study of the Effect of Momentum-Flux Ratio on High-Pressure Nozzle Guide Vane Endwall Cooling Systems
Author:
Affiliation:
1. Department Engineering Science, University of Oxford, Parks Road, Oxford OX1 3PJ, UK e-mail:
2. Department Engineering Science, University of Oxford, Parks Road, Oxford OX1 3PJ, UK
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4037756/6307445/turbo_139_12_121002.pdf
Reference23 articles.
1. Crossflows in a Turbine Cascade Passage;J. Eng. Power,1980
2. The Use of Coloured Smoke to Visualize Secondary Flows in a Turbine Cascade;J. Fluid Mech.,1983
3. Predictions of Endwall Losses and Secondary Flows in Axial Flow Turbine Cascades;ASME J. Turbomach.,1987
4. Experimental and CFD Studies of NGV Endwall Cooling,2013
5. Film Cooling Reasearch on the Endwall of a Turbine Nozzle Guide Vane in a Short Duration Annular Cascade: Part 1—Experimental Technique and Results;ASME J. Turbomach.,1992
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