References
- Nasir, H., Ekkad, S. V., and Acharya, S., 2001, "Effect of Compound Angle Injection of Flat Surface Film Cooling with Large Streamwise Injection Angle," Experimental Thermal and Fluid Science, Vol. 25, Issues. 1-2, pp. 23-29. https://doi.org/10.1016/S0894-1777(01)00052-8
- Walters, D. K., and Leylek, J. H., 2001, "A Detailed Analysis of Film-Cooling Physics: Part I-Streamwise Injection With Cylindrical Holes," Journal of Turbomachinery, Vol. 112, Issue 1, pp. 102-112.
- Yuen, C. H. N., Martinez-Botas, R. F., and Whitelaw, J. H.. 2001, "Film Cooling Effectiveness Downstream of Compound and Fan-shaped Holes." ASME Turbo Expo, New Orleans, Louisiana, 2001-GT-0131.
- Gritsch, M., Colban, W., Schar, H., and Dobbeling, K., 2005, "Effect of Hole Geometry on the Thermal Performance of Fan-Shaped Film Cooling Holes," Journal of Turbomachinery, Vol. 127, pp. 718-725. https://doi.org/10.1115/1.2019315
- Baheri, S., Alavi Tabrizi, S. P., and Jubran, B. A., 2008, "Film cooling effectiveness from trenched shaped and compound holes," Heat Mass Transfer, Vol. 44, Issue 8, pp. 989-998. https://doi.org/10.1007/s00231-007-0341-9
- Brauckmann, D., and Wolfersdorf, J., 2005, "Influence of Compound Angle on Adiabatic Film Cooling Effectiveness and Heat Transfer Coefficient for a Row of Shaped Film Cooling Holes," ASME Turbo Expo, Reno-Tahoe, Nevada, USA, GT2005-68036.
- Japanese Patent Application No. 332530.
- Kusterer, K., Bohn, D., Sugimoto, T., and Tanaka, R., 2006, "Double-Jet Ejection of Cooling Air for Improved Film-Cooling," ASME Turbo Expo 2006, Barcelona, Spain, GT2006-90854.
- Kusterer, K., Bohn, D., Sugimoto, T., and Tanaka, R., 2007, "Influence of Blowing Ratio on The Double-Jet Ejection of Cooling Air," ASME Turbo Expo 2007, Montreal, Canada, GT2007-27301.
- Kusterer, K., Elyas, A., Bohn, D., Sugimoto, T., and Tanaka, R.. 2008, "Double-Jet Film-Cooling for Highly Efficient Film-Cooling with Low Blowing Ratios," ASME Turbo Expo 2008, Berlin, Germany, GT2008-50073.
- Kusterer, K., Elyas, A., Bohn, D., Sugimoto, T., Tanaka, R., and Kazari, M., 2009, "A Parametric Study on the Influence of the Lateral Ejection Angle of Double-Jet Holes on the Film Cooling Effectiveness for High Blowing Ratios," ASME Turbo Expo 2009, Orlando, Florida, USA, GT2009-59321.
- Kusterer, K., Elyas, A., and Bohn, D., 2010, "Film Cooling Effectiveness Comparison Between Shaped and Double Jet Film Cooling Holes In A Row Arrangement," ASME Turbo Expo 2010, Glasgow, UK, GT2010-22604.
- Wang, Z., Liu, J. J., An, B. T., and Zhang, C., 2011, "Effects of Axial Row-spacing For Double-jet Film-cooling On The Cooling Effectiveness," ASME Turbo Expo 2011, Vancouver, Canada, GT2011-46055.
- Heidmann, J. D., 2008, "A Numerical Study of Anti-vortex Film Cooling Designs At High Blowing Ratio," ASME Turbo Expo, Berlin, Germany, GT2008-50845.
- Dhungel, A., Lu, Y., Phillips, W., Ekkad, S. V., and Heidmann, J., 2007, "Film Cooling From A Row of Holes Supplemented With Anti Vortex Holes," ASME Turbo Expo, Montreal, Canada, GT2007-27419.
- CFX-11.0 Solver Theory, Ansys inc,. 2006.
- Bardina, J. E., Huang, P. G., and Coakley, T. J., 1997, "Turbulence Modeling Validation,", AIAA 97-2121.
- Lee, K. D., and Kim, K. Y., 2011, "Surrogate based optimization of a laidback fan-shaped hole for film-cooling," International Journal of Heat and Fluid Flow, Vol. 32, Issue 1, pp. 226-238. https://doi.org/10.1016/j.ijheatfluidflow.2010.08.007
- Lee, K. D., Choi, D. W., and Kim, K. Y., 2013, "Optimization of Ejection Angles of Double-jet Film-cooling Holes Using RBNN Model", International Journal of Thermal Sciences, Vol. 73, pp. 69-78. https://doi.org/10.1016/j.ijthermalsci.2013.05.015
- Baheri, S., Alavi Tabrizi,. S. P., and Jubran, B. A., 2008, "Film cooling effectiveness from trenched shaped and compound holes," Heat Mass Transfer, Vol. 44, pp. 989-998. https://doi.org/10.1007/s00231-007-0341-9
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