COMPUTER PROGRAMS; FILM COOLING; FINITE VOLUME METHOD; HEAT TRANSFER; HOLES (MECHANICS); LEADING EDGES; MASS FLOW; MULTIGRID METHODS; NAVIER-STOKES EQUATION; STAGNATION PRESSURE; STAGNATION TEMPERATURE; THREE DIMENSIONAL FLOW; TURBINE BLADES; VISCOUS FLOW; ADIABATIC EQUATIONS; CARTESIAN COORDINATES; COMPUTATIONAL FLUID DYNAMICS; HEAT TRANSFER COEFFICIENTS; HOLE GEOMETRY (MECHANICS); PRESSURE EFFECTS; PRESSURE MEASUREMENT; RUNGE-KUTTA METHOD; TEMPERATURE EFFECTS; TEMPERATURE MEASUREMENT; THREE DIMENSIONAL MODELS; TURBULENCE MODELS;
机译:薄膜冷却孔位置对涡轮叶片前缘撞击/扩散冷却的流动和传热特性的影响
机译:透平叶片冷却对涡轮叶片传热的影响
机译:对称涡轮叶片模型前沿的薄膜冷却的三维流动和传热计算
机译:包含共轭传热效果的模拟膜冷透平涡轮叶片前缘的数值模拟
机译:在高转数下在燃气涡轮叶片的前缘和后缘冷却通道中的热传递。
机译:燃气轮机叶片前缘旋流膜冷却的共轭传热研究
机译:吹气比对燃气轮机叶片前缘薄膜冷却结构中薄膜冷却效率和传热系数影响的实验和数值研究
机译:前缘薄膜冷却对涡轮叶片传热的影响