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1·The paper analysis control requires of the axial flow compressor.

分析了轴流压缩机工况的控制要求和控制方案。

2·A method for predicting the off design performance of an axial flow compressor is presented.

本文介绍一种轴流压气机非设计性能的预测方法。

3·This article investigates the nonlinear dynamic characteristics and stability of an axial flow compressor with tip clearance and ball bearings.

研究叶尖气隙和滚动轴承共同作用下轴流压缩机的非线性动力特性及稳定性。

4·A new three-dimensional aerodynamic stability model for an axial flow compressor to study the effects of radial disturbance on the rotating stall is presented.

给出了考虑压气机径向扰动对失速影响的轴流压气机三维气动稳定性模型。

5·A stage - by - stage simulation method is introduced for analysis of inlet total pressure distortion effect on the multistage axial flow compressor characteristics.

介绍了1种分析进口总压畸变对多级轴流压气机特性影响的逐级模拟方法。

6·Finally, the total loss distribution along the blade span of the axial flow compressor is estimated according to an improved end wall loss model and a shock loss model.

再应用改进了的端壁损失和激波损失模型，最终算出轴流压气机设计点损失沿叶高的分布规律。

7·When applied to a certain axial flow compressor, the criterion is proved to be precise, reliable and rapid enough to be used in the early detection of rotating stall signal.

对某轴流式压气机压力测量信号的分析结果表明，该判据是准确、可靠和快速的，可以用于旋转失速信号的早期检测。

8·The hub treatment with a circumferential groove was tested on the stator hub and compared with the casing treatment over the rotor tip for a single stage axial flow compressor.

在单级轴流压气机上，用周向槽式处理机匣在静子内径处进行轮毂处理，与转子尖部机匣处理作类比。

9·The characteristics of static pressure changing at stage exits of a multi-stage axial flow compressor relative to the design points at several typical operating modes are investigated.

对多级轴流式压气机在几个典型工况下各级静压相对于设计点静压的变化特性进行了研究。

10·In this paper, virtual prototype technology of turbo-machinery, multistage axial flow compressor numerical simulation, and integrated design of turbo-machinery and engine have been introduced.

介绍了叶轮机虚拟样机技术、多级轴流压气机数值仿真和叶轮机与发动机一体化设计。