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- Abstract: A 3D numerical solution of transonic turbulent flowfield inside a compressor rotor is analyzed with a consideration of blade tip clearance. 文摘:借助于考虑叶片顶部间隙的压气机转子内跨音速湍流流场的三维数值解，得到了该转子流场中的复杂涡系与波系结构。
- Optical fiber sensor for blade tip clearance measurement 叶片叶尖间隙测量的光纤传感器
- Experimental Study of the Effect of Blade Tip Clearance on Turbine Performance 间隙尺寸对涡轮叶栅气动性能影响的实验研究
- EFFECTS OF ROTOR BLADE TIP CLEARANCE ON TOTAL AERODYNAMIC PERFORMANCE IN A RADIAL INFLOW TURBINE 叶轮顶部间隙对向心透平总体性能影响的研究
- Development of Rotating Linear Cascade Facility for Simulating Blade Tip Clearance Flow 模拟叶尖间隙流的转动平面叶栅实验方案
- Stability Analysis of Rotor Systems with Gas Exciting Force Caused by Blade Tip Clearance 叶轮偏心引起的气流激振力对转子稳定性影响的分析
- Statistical design for turbine blades tip clearance loss analysis 航空发动机涡轮叶尖间隙损失的统计设计
- blade tip clearance 浆叶端隙
- Analysis of the flow through the blade tip clearances of axial pumps by CFD 轴流泵叶顶间隙流动的计算流体动力分析
- Therefore,for the adjustable blade spiral mixed flow pump,the design of fixed guide blade should be paid attention to and the tip clearance of blade should be rationally selected. 因此，对于可调叶片蜗壳式混流泵应重视固定导叶的设计，合理地选择轮缘间隙的大小。
- The numerical results show that blade cutting causes the development of tip clearance vortices and blade passage blockages, which reduce the flow rate and the work done by the blade. 基于数值计算结果的流场分析表明，叶片磨短后叶顶间隙涡进一步发展，阻塞叶顶流道，使流量锐减，同时降低了叶片顶部区域做功能力。
- tip clearance cavitations on blade flange 轮缘间隙空蚀
- Its h.p.and m.p.sealing glands and blade tip sealing were modified with an American adjustable sealing. 1997年7月在第二次大修中引进了美国布莱登可调式汽封，对其高、中压汽封及叶顶汽封进行改造。
- Based on the above,mechanisms of the influence of tip clearance of rotating blades on aerodynamic-aeroacoustic performance are revealed preliminarily. 初步揭示了非自模化区域内动叶叶尖间隙对气动-声学性能影响的机理。
- With the aid of commercial CFD code CFX, the results of six numerical simulation cases which different tip clearance are presented in this work. 研究动叶顶部间隙泄漏流动对透平级气动性能的影响规律，具有重要的工程应用价值和学术研究意义。
- Venter, S. J. and Kroger, D. G. " The Effect of Tip Clearance on the Performance of an Axial Flow Fan,” Energy Convers. Mgmt, Vol. 33, No. 2, pp. 89-97, 1992. 林育洲，“轴流风扇之数值与实验分析”，国立台湾科技大学机械工程技术研究所硕士论文，1998年7月。
- By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing. 本文给出了一种基于区域分解算法的可考虑动叶顶部间隙和机匣刮削作用的涡轮级计算方法。
- Abstract: By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing. 文摘:本文给出了一种基于区域分解算法的可考虑动叶顶部间隙和机匣刮削作用的涡轮级计算方法。
- The parameter influence of rotor free-wake method was presented, including blade discrete segments, vortices grid density and wake length.Several areas were made from blade root to blade tip. 摘要介绍了自由涡方法中多个参数的影响，包括桨叶离散段数、有弯度翼型的涡网格密度、尾迹的长度。
- The flow separation and great range low energy flow occur at the 10% span range of second rotor blade tip near stall point firstly, which was the main reason for the compressor stall. 在近失速点压气机第二排转子叶片吸力面近尖部10%25叶展范围内，最先出现导致叶片失速的大范围分离和低能堵塞团；
