Computation of leading edge film cooling from a CONSOLE geometry (CONverging Slot hOLE)
Author:
Publisher
Pleiades Publishing Ltd
Subject
Nuclear and High Energy Physics,Radiation
Link
http://link.springer.com/content/pdf/10.1134/S0869864316010042.pdf
Reference33 articles.
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3. A.K. Sinha, D.G. Bogard, and M.E. Crawford, Film-cooling effectiveness downstream of a single row of holes with variable density ratio. ASME J. Turbomachinery, 1991, Vol. 113, P. 442–449.
4. J.C. Han, S. Dutta, and S.V. Ekkad, Gas turbine heat transfer and cooling technology, Taylor & Francis, London, 2000.
5. A. Azzi, M. Abidat, and B.A. Jubran, Film cooling predictions of simple and compound angle injection from one and two staggered rows. Numerical Heat Transfer. Part A: Applications, 2001, Vol. 40, No. 3, P. 273–294.
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