A Novel Antivortex Turbine Film-Cooling Hole Concept
Author:
Affiliation:
1. NASA Glenn Research Center, Cleveland, OH 44135
2. Louisiana State University, Baton Rouge, LA 70803
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.2777194/5845083/031020_1.pdf
Reference29 articles.
1. Film Cooling
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3. Turbine Airfoil Leading Edge Film Cooling Bibliography: 1972–1998;Kercher;Int. J. Rotating Mach.
4. Film Cooling With Large Density Differences Between the Mainstream and the Secondary Fluid Measured by the Heat-Mass Transfer Analogy;Pedersen;ASME J. Heat Transfer
5. The Flow and Film Cooling Effectiveness Following Injection Through a Row of Holes;Foster;ASME J. Eng. Power
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