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- The aerodynamic performance of the aft-loaded and fore-loaded turbine blade was investigated using the linear and annular turbine cascades experiments. 摘要采用平面叶栅和环形叶栅吹风试验对后加载和高负荷前加载叶型的气动性能进行了详细的测量和研究。
- In addition, the efficiency of turbine cascades with pressure difference endwall profiling method have 3.8% improvement. 采用压差法造型的叶栅流道，其效率提高了3.;8%25。
- For investigating the aerodynamic character of the turbine cascades, understanding the detail flow in turbine cascades, the computational investigation was applied on some type turbine guide vane. 为了详细研究涡轮叶栅的气动特性,深入了解涡轮叶栅流道内的气体流动,对某型涡轮导向叶栅内的流场结构进行了数值模拟。
- Topology and Vortex Structures of Turbine Cascade with Different Tip Clearances. 在不同叶顶间隙下涡轮叶栅的拓扑与旋涡结构。
- Abstract: The exit flow fields of a turbine cascade with or without the front guide vanes were investigated. 文摘:详细测量了平行进口端壁附面层与设前导叶两种进口条件下某涡轮叶栅的出口流场。
- Theexperimental results show that there are s trong secondary flow and a complex series of vortices in turbine cascade. 实验结果表明：涡轮叶栅中有强烈的二次流动，并存在复杂的涡系；
- Moore H,Gregory-Smith D G.Turbulence and Transition in Secondary Flows in a Turbine Cascade[R].AGRAD-CP-571,1995. 向传国;曾军;康勇.;某核心机出口整流支板设计和流场分析[C]
- A two-dimensional, compressible flow model for loss created by the mixing behind the turbine cascade with coolant injection is presented, based on the theory developed by Denton. 基于Denton的尾缘流动理论 ,发展了一种考虑冷气喷射的二维、可压涡轮叶栅尾缘混合损失模型 ,研究了涡轮叶栅尾缘损失的特征 ,定量评估了影响尾缘损失的各种参数。
- Detailed aerodynamic measurements were carried out in the passage of a large-scale low speed turbine cascade with single row injection on the endwall upstream of leading edge. 摘要在大尺寸低速平面叶栅风洞中，对前缘上游有单排气膜孔的涡轮导向叶栅端壁气膜冷却进行了气动实验。
- Planar cascade with nonthickness straight-line airfoils, Hobson's transonic turbine cascade andasubsonic turbine cascade from Lewis Research center are computated and checked. 边界条件处理宜试用高精度格 式；
- Simulated Annealing Algorithm Applied to Optimize Design of Turbine Cascades 模拟退火算法在透平叶栅多目标优化设计中的应用
- Hotwire-based Experimental Study of Secondary Flows in Turbine Cascades 涡轮叶栅二次流的热线实验研究
- Effect of Different Sweep Depth on Energy Losses of Turbine Cascades 掠高变化对涡轮叶栅能量损失的影响
- Numerical Simulation of Transonic Flow Field in Two Turbine Cascades 两个涡轮叶栅跨声速流场的数值模拟
- The nucleating flows in Laval nozzle and 2D turbine cascade are simulated. By comparison with experimental data, good agreement between calculated and experimental surface pressure is obtained and the distributions of many flow parameters are displayed. 计算了Moore喷管和Bakhtar叶栅凝结流，并与实验数据进行了对比，得到了很好的计算与实验压力的一致性及丰富的流动参数分布。
- The river fell in a series of cascades down towards the lake. 河形成阶梯状瀑布泻入湖中。
- Xiang Anding,Zhu Huiren,Liu Songling,et al.Discharge coefficient measurements for film cooling holes on blade surface in a turbine cascade[J].Journal of Propulsion Technology,2003,24(3):216-218. [6]向安定;朱惠人;刘松龄;等.;涡轮导向叶片表面气膜孔流量系数的实验研究[J]
- The gas turbine feeds on the fuel it pumps. 燃气轮机以它所抽入的燃料为能源。
- Measurements of flow passage inside a rectangular turbine cascade with large turning angle while cooling-air injection upstream from three different rows at leading edge were performed. 摘要对具有前缘逆主流不同位置喷射冷气的大转折角气冷涡轮直叶栅进行了详细的流道内部测量。
- Based on the mechanism of secondary flow formation and development in a turbine cascade, SINE function and polynomial function were applied to develop a non-axisymmetric endwall profiling method. 摘要根据叶栅内部二次流形成和发展的机理，应用正弦函数和多项式函数建立了一种叶栅非轴对称端壁成型方法。
