1. Z.X. Wen, D.X. Zhang, S.W. Li, et al., Anisotropic creep damage and fracture mechanism of nickel-base single crystal superalloy under multiaxial stress. J. Alloys Compd. 692, 301–312 (2017)
2. D. Lakehal, G.S. Theodoridis, W. Rodi, Three-dimensional flow and heat transfer calculations of film cooling at the leading edge of a symmetrical turbine blade model. Int. J. Heat Fluid Flow 22(2), 113–122 (2001)
3. Youn J. Kim, S.M. Kim, Influence of shaped injection holes on turbine blade leading edge film cooling. Int. J. Heat Mass Transf. 47(47), 245–256 (2004)
4. H. Yi et al., Influence of the surface curvature of a blade profile on its discrete hole air-film cooling performance. Reneng Dongli Gongcheng/J. Eng. Thermal Energy Power 27(2), 149–153 (2012)
5. Scot K. Waye, D.G. Bogard, High-resolution film cooling effectiveness comparison of axial and compound angle holes on the suction side of a turbine vane. J. Turbomach. 129(2), 195–203 (2007)