Numerical approach to hole shape effect on film cooling effectiveness over flat plate including internal impingement cooling chamber

International Journal of Heat and Mass Transfer - Tập 49 - Trang 919-938 - 2006
Jr-Ming Miao1, Chen-Yuan Wu2
1Department of Mechanical Engineering, Chung Cheng Institute of Technology, National Defense University, 335 Taoyuan, Taiwan, ROC
2Graduate School of Defense Science Studies, Chung Cheng Institute of Technology, National Defense University, 335 Taoyuan, Taiwan, ROC

Tài liệu tham khảo

Han, 2000 Ammari, 1990, The effect of density ratio on the heat transfer coefficient from a film-cooled flat plate, ASME J. Turbomach., 112, 444, 10.1115/1.2927679 Goldstein, 1999, Film cooling effectiveness and mass/heat transfer coefficient downstream of one row of discrete holes, ASME J. Turbomach., 121, 225, 10.1115/1.2841305 Baldauf, 2001, High-resolution measurements of local heat transfer coefficients from discrete hole film cooling, ASME J. Turbomach., 123, 749, 10.1115/1.1387245 Baldauf, 2001, High-resolution measurements of local effectiveness from discrete hole film cooling, ASME J. Turbomach., 123, 758, 10.1115/1.1371778 Loftus, 1983, The effect of temperature ratios on the film cooling process, ASME J. Eng. Power, 105, 615, 10.1115/1.3227461 Ligrani, 1989, Effects of embedded vortices on film-cooled turbulent boundary layers, ASME J. Turbomach., 111, 71, 10.1115/1.3262239 Cho, 1995, Heat (mass) transfer and film cooling effectiveness with injection through discrete holes: Part I—Within holes and on the back surface, ASME J. Turbomach., 117, 440, 10.1115/1.2835680 Leylek, 1994, Discrete-jet film cooling: a comparison of computational results with experiments, J. Turbomach., 116, 358, 10.1115/1.2929422 Hyams, 2000, A detailed analysis of film cooling physics. Part III: Streamwise injection with shaped holes, ASME J. Turbomach., 122, 122, 10.1115/1.555435 Bell, 2000, Film cooling from shaped holes, ASME J. Heat Transfer, 122, 224, 10.1115/1.521484 Gritsch, 2000, Film-cooling holes with expanded exits: near-hole heat transfer coefficients, Int. J. Heat Fluid Flow, 21, 146, 10.1016/S0142-727X(99)00076-4 Jung, 2000, Effects of orientation angles on film cooling over a flat plate: boundary layer temperature distributions and adiabatic film cooling effectiveness, ASME J. Turbomach., 122, 153, 10.1115/1.555437 Yu, 2002, Film cooling effectiveness and heat transfer coefficient distributions around diffusion shaped holes, ASME J. Turbomach., 124, 820 Behbahani, 1983, Local heat transfer to staggered arrays of impingement circular air jets, ASME J. Eng. Power, 105, 354, 10.1115/1.3227423 Huang, 1998, Detailed heat transfer distributions under an array of orthogonal impinging jets, J. Thermophys. Heat Transfer, 12, 73, 10.2514/2.6304 Azad, 2000, Impingement heat transfer on dimpled surfaces using a transient liquid crystal technique, J. Thermophys. Heat Transfer, 14, 186, 10.2514/2.6530 S.J. Downs, E.H. James, Jet impingement heat transfer-a literature survey, ASME Paper 87-HT-35, 1987. Viskanta, 1993, Heat transfer to impingement isothermal gas and flame jets, Exp. Thermal Fluid Sci., 6, 113, 10.1016/0894-1777(93)90022-B Cho, 2001, Enhancement of film cooling performance using a shaped film cooling hole with compound angle injection, JSME Int. J. Ser. B, 44, 99, 10.1299/jsmeb.44.99 Schiele, 2000, Gas turbine heat transfer: past and future challenges, J. Propulsion Power, 16, 583, 10.2514/2.5611 Ai, 2001, The selection criterion of injection temperature pair for transient liquid crystal, Int. J. Heat Mass Transfer, 44, 1389, 10.1016/S0017-9310(00)00153-8 Wilcox, 1993 Nasir, 2000, Effect of compound angle injection on flat surface film cooling with large streamwise injection angle, Proceeding of the 8th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2, 763 Walters, 2000, A detailed analysis of film-cooling physics. Part I—Streamwise injection with cylindrical holes, ASME J. Turbomach., 122, 102, 10.1115/1.555433