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1·Reason of error generated when axial compressor and TRT blades processed by profiling is analyzed.

分析了用靠模法加工轴流压缩机叶片及能量回收透平膨胀机叶片时产生误差的原因。

2·Then the deposition characteristic of different particle diameters in the blade cascade of the axial compressor was obtained.

在此基础上，研究了轴流压缩机叶栅内不同直径粒子在叶片压力面和吸力面的沉积规律；

3·The internal flow field of a single-stage axial compressor is analyzed using a fast full 3-D viscous flow calculating method.

采用一种快速求解三维粘性流场的计算方法求解轴流压气机的内部流场及全工况特性。

4·The unsteady surface pressure on stator blade of an axial compressor was measured by means of mounting micro-sensors on blades surface.

本文对一台单级轴流压气机静子叶片非定常表面压力进行了测量。

5·The influence of tip clearance on overall performance and detailed flow structure in tip region of an axial compressor rotor was investigated.

研究了顶部间隙对压气机转子总性能及内部流场的影响。

6·Results show that the frequency and rotating direction of inlet distortion are most important factors affecting stability of axial compressor.

在低速大尺寸单级压气机实验器上，实验研究了动态进气畸变对压气机稳定边界的影响。

7·This paper describes the initial experimental results of aeroelastic instability of BF-1 rotors on a transonic axial compressor facility at BIAA.

本文介绍了在跨音压气机试验台上对BF - 1系列转子开展气动弹性失稳的实验研究工作。

8·The full-scale three-dimensional flow centrifugal stage test conducted on an axial compressor test rignecessitates a test rig compatibility design.

在轴流压气机试验台上进行全尺寸三元流离心级的试验，需进行适台设计。

9·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。

10·The multi-stage axial compressor performance was measured using a streamline curvature method based on two-dimension(axisymmetric) mathematical model.

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。