[1] R. J. Goldstein, E. R. G. Eckert, F. Burggraf, Effects of Hole Geometry and Density on Three Dimensional Film Cooling, Int. J. Heat Mass Transfer, Vol. 17, pp. 595-607, 1974.
[2] M. Gritsch, A. Schulz, S. Wittig, Adiabatic Wall Effectiveness Measurements of Film Cooling Holes with Expanded Exits, Journal of Turbomachinery, Vol. 120, pp. 549–556, 1998.
[3] M. Gritsch, W. Colban, H. Schar, K. Dobbeling, Effect of Hole Geometry on the Thermal Performance of Fan-Shaped Film Cooling Holes, ASME Journal of Turbomachinery, Vol. 127, pp. 718-725, 2005
[4] M. E. Taslim, A. Khanicheh, Film Effectiveness Downstream of a Row of Compound Angle Film Holes, Journal of Heat Transfer, Vol. 127, No. 4, pp. 434-440, 2005.
[5] Z. Gao, D. P. Narzary, J. Han, Film Cooling on a Gas Turbine Blade Pressure Side or Suction Side with Axial Shaped Holes, International Journal of Heat and Mass Transfer, Vol. 51, pp. 2139-2152, 2008.
[6] C. Saumweber, A. Schulz, Effect of Geometry Variations on the Cooling Performance of Fan-Shaped Cooling Holes, Universität Karlsruhe, Karlsruhe, Germany, pp. 905-919, 2008.
[7] W. F. Colban, K. A. Thole, D. Bogard, A Film Cooling Correlation for Shaped Holes on a Flat-Plate Surface, Journal of Turbomachinery,Vol. 133, No. 1, 2011.
[8] C. Q. Nguyen, P. L. Johnson, B. C. Bernier, S. H. Ho, J. S. Kapat, Comparison of FIlm Effectiveness and Cooling Uniformity of Conical and Cylindrical-Shaped Film Hole With Coolant-Exit Temperature Correction, Journal of Thermal Science and Engineering Application, Vol. 3, pp. 031011-1 -9, 2011.
[9] K. D. Lee, K. Y. Kim, Optimization of a Cylindrical Film Cooling Hole Using Surrogate Modeling, Numer.Heat Trans.A, Vol. 55, pp. 362–380, 2009.
[10] K. D. Lee, K. Y. Kim, Shape Optimization of a Fan-Shaped Hole to Enhance Film-Cooling Effectiveness, International Journal of Heat and Mass Transfer,Vol. 53, pp.2996-3005, 2010.
[11] K. D. Lee, S. M. Kim, K. Y. Kim, Multi-Objective Optimization of Film-Cooling Holes Considering Heat Transfer and Aerodynamic Loss, Proceedings of ASME Turbo Expo, Paper No. GT2011-45402, Vancouver, British Columbia, Canada, June 6-10, 2011.
[12] E. C. Ayoubi, Three-Dimensional Aero-Thermal Optimization of Film Cooling in a High Pressure Turbine, Phd Thesis, Department of Mechanical and Industrial Engineering, Concordia University, Montreal, Quebec, Canada, 2014.
[13] K. Kusterer, J. Dickhoff, T. Sugimoto, Multi-Objective Pareto Optimization of the NEKOMIMI Film Cooling Technology by Utilization of the SHERPA Algorithm, Proceedings of International Gas Turbine Congress, Tokyo, Japan, 15-20, 2015.
[14] Zolfagharian, Optimaization of Turbine Blade Cooling by Using of Combinational Methods, Semnan University, Ms.Thesis 198945, 1993.
[15] H. R. Rezaei, R. P. Gupta, G. W. Bryant, J. T. Hart, G. S. Liu, C. W. Bailey, T. F. Wall, S. Miyamae, K. Makino, Y. Endo, Thermal Conductivity of Coal Ash and Slags and Models Used, Fuel, pp. 1697-1710, 2000.
[16] J. Han, S. Dutta, S. Ekkad, Gas Turbine Heat Transfer and Cooling Technology, New York: Taylor & Francis, 2000.