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- An experimental comparison research of endwall heat transfer characteristics was conducted in the complex passages of turbine blade trailing edge by using thermochromic liquid crystal method. 摘要采用热色液晶测温法,测量了涡轮叶片尾缘带隔板的复合通道的温度场,分析了射流冲击强化扰流柱通道内换热的机理,讨论了两通道间隔板的不同开孔结构对换热的影响。
- Heat transfer in complex passages of turbine blade trailing edge 涡轮叶片尾缘复合通道的换热
- turbine blade trailing edge 叶片尾缘
- In this paper, heat transfer and fluid flow in passage for trailing edge of turbine blade with pin-fin arrays is studied numerically. 本文应用湍流模型对涡轮叶片尾缘针肋通道的换热与流动进行了二维数值模拟研究。
- Mixing process in symmetry trailing edge slot for a turbine blade 喷气流与栅后流场掺混及干扰效应的探讨
- Study of Water-erosion Characteristics and Fatigue Crack Propagation of Last Stage Moving Blade Trailing Edge of a Steam Turbine 汽轮机末级动叶片出口边水蚀特性及疲劳裂纹扩展的研究
- INVESTIGATION OF THE BEST AUGMENTED HEAT TRANSFER OF PIN-FIN ARRAYS IN PASSAGE FOR TRAILING EDGE OF TURBINE BLADE 叶片尾缘内冷通道中最佳强化传热的针肋排列结构研究
- Experiment and Numerical Simulation Investigation of Turbine Blade with Trailing Edge Ejection 涡轮叶片尾缘开缝喷气的数值模拟和试验研究
- Influence of slot treatment on flow performance of blade trailing edge 开槽处理技术对叶片尾缘气流流动特性的影响
- Theoretical Research on Shape of Pin-fin in Cooling Blade Trailing Edge 涡轮叶片尾缘扰流柱最佳形状的研究
- EFFECT OF TRAILING EDGE EJECTION OF TURBINE BLADES ON HEAT TRANSFER OF COOLING PASSAGE WITH STAGGERED PIN FINS 涡轮叶片尾缘出流对带叉排扰流柱阵列的内冷通道传热特性的影响
- Wuxi Turbine Blade Works Co., Ltd. 无锡透平叶片有限公司。
- blade trailing edge 叶片出汽边
- Measurements of heat transfer and pressure drop in the short pin fin array used in trail cooling channel of turbine blade have been performed. 采用放大的模型对装有五排短扰流柱的涡轮叶片尾缘的冷却通道的流阻特性及通道端壁表面上的局部换热系数进行了测量,重点研究了扰流柱直径及形状的影响。
- The movement occurs on the trailing edge of the pulse. 移动是在脉冲的下降沿产生的。
- Measurements of heat transfer and pressure drop in the short pin-fin array used in trail cooling channel of turbine blade have been performed. 采用放大的模型对装有五排短扰流柱的涡轮叶片尾缘的冷却通道的流阻特性及通道端壁表面上的局部换热系数进行了测量,重点研究了扰流柱直径及形状的影响。
- A variable control surface on the trailing edge of an aircraft wing, used primarily to increase lift or drag. 襟翼飞机后翼上最初用来增加上升力或拖力的可灵活控制的辅助翼
- Leading edge and trailing edge means the function of the dimmer. 飞机螺旋桨的前边缘和机翼后边缘是最能够反应调光器的功能的。
- KEY WORDS Anisotropic, Constitutive model, Viscoplastic, Turbine blade. 关键词:正交异性,本构模型,粘塑性,涡轮叶片
- Boundary layer characteristics at the trailing edge of a tiltrotor blade model were measured using a flattened pitot probe and a single hot wire. 本研究以二体势能函数建立一套接触式原子力显微镜定力模式之模拟奈米级量测模型。