[1] Bohn D, et al. Prediction of the Film-Cooling Effectiveness in Gas Turbine Blades Using a Numerical Model for the Coupled Simulation of Fluid Flow and Diabatic Walls. Proceedinf of the 12thInternational Symposium on Air Breathing Engines,1995.1150~1159

[2] Bohn D, et al. 3-D Numerical Simulation of the Flow Through a Turbine Blade Cascade with Cooling Injection at the Leading Edge. ASME Paper 97-GT-247,1997

[3] Haselhause A, Vogel D T. Nuimerical Simulation of Turbine Blade Cooling with Respect to Blade Heat Conduction and Inlet Temperature Profiles. AIAA Paper 95-3041,1995

[4] Kao K H, Liu M S. On the Application of Chimera/Unstructed Hybrid Grids for Conjugate Heat Transfer. ASME Paper 96-GT-165,1996

[5] V Michelassi, et al. Aerodynamic Performance of A Transonic Turbine Guide Vane with Trailing Edge Coolant Ejection Part II Numerical Approach.ASME Paper 94-GT-248, 1994

[6] 陈浮,王仲奇,冯国泰. 跨音速旋转气冷涡轮叶栅流场计算研究.中国工程热物理学会热机气动热力学学术会议,杭州,1998

[7] W N Dawes. Toward Improved Throughflow Capability:The Use of Three-Dimensional Viscous Flow Solvers in a Multistage Environment. ASMEJ of Turbomachinery, 1992, 114: 8~17

[8] J D Denton. The Calculation of Three Dimensional Viscous Flow through Multistage Turbomachines. ASMEJ of Turbomachinery, 1992, 114:18~26

[9] AdamczykJJ, et al. Simulation of Viscous Flow within a Multistage Turbine. ASMEJ of Turbomachinery, 1992.112

[10] C H Sieverding, et al. Investigation of the Flow Field Downstream of A Turbine Trailing Edge Cooled Nozzle Guide Vane. ASME Paper 94-GT-209,1994