Improvement of film cooling effectiveness with a small downstream block body
Author:
Publisher
Pleiades Publishing Ltd
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1134/S0021894416040106.pdf
Reference20 articles.
1. J. C. Han, S. Dutta, S. V. Ekkad, Gas Turbine Heat Transfer and Cooling Technology (Taylor and Francis, London, 2000).
2. K. Thole, M. Gritsch, A. Schulz, and S. Wittig, “Flowfield Measurements for Film-Cooling Holes with Expanded Exits,” ASME, J. Turbomachinery 120, 327–336 (1998).
3. M. Gritsch, A. Schulz, and S. Wittig, “Adiabatic Wall Effectiveness Measurements of Film-Cooling Holes with Expanded Exits,” ASME, J. Turbomachinery 120, 549–556 (1998).
4. A. Azzi, M. Abidat, and B. A. Jubran, “Film Cooling Predictions of Simple and Compound Angle Injection from One and Two Staggered Rows,” Numer. Heat Transfer, Part A 40, 273–294 (2001).
5. H. Nasir, S. V. Ekkad, and S. Acharya, “Effect of Compound Angle Injection on Flat Surface Film Cooling with Large Streamwise Injection Angle,” Experiment. Thermal Fluid Sci. 25 (1/2), 23–29 (2001).
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