The effect of turbulence intensity on film cooling of gas turbine blade from trenched shaped holes
Author:
Publisher
Springer Science and Business Media LLC
Subject
Fluid Flow and Transfer Processes,Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s00231-011-0938-x.pdf
Reference16 articles.
1. Garg VK (1999) Heat transfer on a film-cooled rotating blade. NASA Rep, NASA/CR-1999–209301, NASA Glenn Research Center, Cleveland, OH
2. Azzi A, Abidat M, Jubran BA, Theodoridis GS (2001) Film cooling predictions of simple and compound angle injection from one and two staggered rows. Numer Heat Transf A 40:273–294
3. Sarkar S, Bose TK (1995) Comparison of different turbulence models for prediction of slot-film cooling: flow and temperature field. Numer Heat Transf B 28:217–238
4. Ou S, Han JC (1994) Leading edge film cooling heat transfer through one row of inclined film slots and holes including mainstream turbulence effects. ASME J Heat Transf 116:561–569
5. Mehendale AB, Han JC (1992) Influence of high mainstream turbulence on leading edge film cooling heat transfer: effect of film hole spacing. Int J Heat Mass Transf 35(10):2593–2604
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