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- THE EFFECT OF TIP CLEARANCE GAP SIZE AND WALL ROTATION ON THE PERFORMANCE OF A LOW-SPEED AXIAL COMPRESSOR ROTOR 叶顶间隙大小和壁面相对运动对低速轴流压气机孤立转子性能的影响
- Development of Three-Dimensional Turbulent Flow Field at Exit of an Axial Compressor Rotor Passage 压气机转子出口流场的发展及三维紊流特性
- Three-Dimensional Mean Flow Field at Both Inlet and Exit of an Isolated Axial Compressor Rotor Passage in Different Conditions 单转子轴流压气机不同状态下进出口三维时均流场
- Axial compressor rotor 轴流压气机转子
- The unsteady surface pressures on the rotor blades of a single-stage low-speed axial compressor were measured by means of mounting micro-sensors on the surface the blades. 摘要为了研究上游叶片尾迹对轴流压气机转子叶片非定常表面压力的影响，采用在叶片表面埋设微型压力传感器的方法，测量了一个单级低速轴流压气机转子叶片的非定常压力分布。
- This paper presents an experimental investigation of the transportation of the rotor tip leakage vortex and the rotor wake in an axial compressor stator passage. 结果表明,转子叶尖泄漏涡和转子尾迹周期地扫过静子通道尖区,导致该区出现周期性的流动阻塞和脉动。
- 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。
- Free moving vanes are inserted into slots in the compressor rotor, which is mounted eccentricly in the pump cylinder. 可自由移动的页片被插入压缩机转子槽内;.;(转子被偏心装在泵缸体内)。
- The IGV/rotor interaction phenomenon in a one stage low speed axial compressor was investigated experimentally. 对于一台单级低速轴流压气机内的导叶／转子干涉现象进行了实验研究。
- Zielinski M,Ziller G.Non-Contact Vibration Measurements on Compressor Rotor Blades[J]. 方志强.;段发阶等
- Operating data chart of the AV-series axial compressor with all the stator blades adjustable(Medium:Air). AV型系列轴流压缩机（全静叶可调）性能参数表（介质：空气）
- In order to improve axial compressor efficiency,a new high performance rotating blade is required. 为了提高轴流压气机的效率,需要研究一种新的高性能的转子叶片。
- We developed a quick three dimensional computing procedure used for multistage axial compressor. 发展了一套用于多级轴流式压气机的快速三维计算程序。
- A numerical optimization code was developed and applied to the optimization design of a circumferentially curved transonic compressor rotor. 优化结果表明压气机动叶弯曲可以有效地改变流场内的三维激波结构，削弱尾迹损失。
- To implement stall margin customizing,two-dimensional performance prediction method of axial compressor for stall margin customizing was developed. 为实施裕度定制,本文开发了能够体现裕度定制思想的轴流压气机二维特性预估方法。
- Abstract: Unsteady static pressure field on the tip endwall of an axial-flow compressor rotor passage was measured using a micro high freqnency pressure transducer. 文摘:用高频压力传感器测量了低速单级压气机转子叶尖动态压力场。
- The generation of repeating stage flow pattern in a multistage axial compressor and a simulation model of its flow field are investigated. 本文对轴流压气机多级环境中存在的重复级流动现象的建立及其在流场数值模拟中的应用进行了研究。
- Unsteady static pressure field on the tip endwall of an axial-flow compressor rotor passage was measured using a micro high freqnency pressure transducer. 用高频压力传感器测量了低速单级压气机转子叶尖动态压力场。
- The multi-stage axial compressor performance was measured using a streamline curvature method based on two-dimension (axisymmetric) mathematical model. 摘要采用二维（轴对称）数学模型，应用流线曲率法求解多级轴流压气机特性。
- Egorov I N. Optimization of multistage axial compressor in a gas turbine engine system[ J]. ASME paper, 92 - GT - 424 1992. 鞠云峰译.;轴流气机采用人工智能和数值优化技术初步设计[J]
