仿真结果表明,当压气机叶片表面粗糙度增大时,压气机主要特性参数都不同程度的减小,使压气机总体性能下降。
The simulation results show that the performance parameters are decreased in various degree and the compressor general performance is reduced when the roughness of the blade surface is increased.
并采取在静子叶片表面埋入微型压力传感器的方法,分析了压气机流场的动态压力特性。
The pressure dynamic proceedings of three cross-section of the stator surface had been investigated to understand the flow structure in a compressor.
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。
The unsteady surface pressure on stator blade of an axial compressor was measured by means of mounting micro-sensors on blades surface.
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