A Detailed Study of the Interaction Between Two Rows of Cooling Holes
Author:
Affiliation:
1. Osney Thermo-Fluids Laboratory, Department of Engineering Science, Oxford University, Oxford OX2 0ES, UK e-mail:
2. CFD Methods, Rolls-Royce PLC, Derby DE24 8BJ, UK e-mail:
3. Turbine Systems, Rolls-Royce PLC, Bristol BS34 7QE, UK e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4038833/6308262/turbo_140_04_041008.pdf
Reference33 articles.
1. Fundamental Gas Turbine Heat Transfer;ASME J. Therm. Sci. Eng. Appl.,2013
2. Adiabatic Wall Effectiveness Measurements of Film-Cooling Holes With Expanded Exits;ASME J. Turbomach.,1998
3. Effect of Geometry Variations on the Cooling Performance of Fan-Shaped Cooling Holes;ASME J. Turbomach.,2012
4. A Detailed Analysis of Film Cooling Physics—Part II: Compound-Angle Injection With Cylindrical Holes;ASME J. Turbomach.,2000
5. A Detailed Analysis of Film-Cooling Physics: Part I—Streamwise Injection With Cylindrical Holes
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