Computational Simulation of Deposition in a Cooled High-Pressure Turbine Stage With Hot Streaks
Author:
Affiliation:
1. Aerospace Research Center, The Ohio State University, Columbus, OH 43235 e-mail:
2. NASA Glenn Research Center, Cleveland, OH 44135; The Ohio State University, Columbus, OH 43210
Abstract
Funder
U.S. Department of Energy
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4036008/6408260/turbo_139_09_091005.pdf
Reference37 articles.
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3. Film Cooling Effectiveness and Heat Transfer Near Deposit-Laden Film Holes;ASME J. Turbomach.,2011
4. Effect of Particle Size Distribution on Particle Dynamics and Blade Erosion in Axial Flow Turbines;ASME J. Eng. Gas Turbines Power,1991
5. Turbine Blade Surface Deterioration by Erosion;ASME J. Turbomach.,2004
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