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Nguồn tham khảo
| Tài liệu tham khảo | Loại | Chi tiết | ||
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| [1] Muller, S. D., Walther, J. H., and Koumoutsakos, P. D., 2001, “Evolution Strategies for Film Cooling Optimization,”AIAA J., 39(3), pp. 537–539 | Sách, tạp chí |
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| [2] Nowak, G., and Wroblewski, W., 2011, “Optimization of Blade Cooling System With Use of Conjugate Heat Transfer Approach,”Int. J. Therm. Sci., 50(9), pp. 1770–1781 | Sách, tạp chí |
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| [3] Dennis, B., Egorov, I., Dulicravich, G., and Yoshimura, S., 2003, “Optimization of a Large Number Coolant Passages Located Close to the Surface of a Turbine Blade,” Proceedings of Turbo Expo 2003, Atlanta, June 16–19, Paper No. GT2003-38051 | Sách, tạp chí |
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| [4] Haasenritter, A., and Weigand, B., 2004, “Optimization of the Rib Structure Inside a 2D Cooling Channel,”ASMEPaper No. GT2004-53187 | Sách, tạp chí |
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| [5] Yingjie Song et.all, 2014 ” Multi-Objective and Multi-Disciplinary “ Optimization of Gas Turbine Blade Profile and Cooling System Using Conjugate Heat Transfer Analysis”, International Gas Turbine Institute, pp. 978-0-7918- 4561-5 | Sách, tạp chí |
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| [8]. Schmidt, D. L., Sen., B., 1996, “Film Cooling With Compound Angle Holes: Adiabatic Effectiveness,” ASME Journal of Turbo machinery, Vol.118, pp. 807–813 | Sách, tạp chí |
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| [6] Facchini, B., Magi, A., Greco, A.S.D.. Conjugate heat transfer simulation of a radially cooled gas turbine vane. Proceedings of ASME TurboExpo 2004;(GT2004-54213) | Khác | |||
| [7] Laskowski, G.M., Ledezma, A.G., Tolpadi, A.K., Ostrowsky, M.. Cfdsimulations and conjugate heat transfer analysis of a high pressure turbine vane utilizing different cooling configurations. 12th ISROMAC Symposium, 17- 22 February 2008, Honolulu, Hawaii 2008;IS ROMAC12-2008-20065 | Khác |
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