Effects of Coolant Density, Specific Heat Capacity, and Biot Number on Turbine Vane Cooling Effectiveness
Author:
Affiliation:
1. Department of Engineering Science, University of Oxford, Parks Road, Oxford OX1 3PJ, UK e-mail:
2. Department of 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/10.1115/1.4037029/6306492/turbo_139_11_111005.pdf
Reference24 articles.
1. The Effect of Temperature Ratios on the Film Cooling Process;J. Eng. Power,1983
2. Effects of Hole Geometry and Density on Three-Dimensional Film Cooling;Int. J. Heat Mass Transfer,1974
3. Film Cooling With Large Density Differences Between the Mainstream and the Secondary Fluid Measured by the Heat-Mass Transfer Analogy;ASME J. Heat Transfer,1977
4. Effects of Density Ratio on the Hydrodynamics of Film Cooling;ASME J. Turbomach.,1990
5. Film-Cooling Effectiveness Downstream of a Single Row of Holes With Variable Density Ratio;ASME J. Turbomach.,1991
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