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。
Experimental tests have been carried out to investigate the influence of inlet distortion on compressor stability margin in a low speed single stage research 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。
Results show that the frequency and rotating direction of inlet distortion are most important factors affecting stability of axial compressor.
在吊舱进气道进口安装扰流板进行试验，研究扰流板进气畸变的影响因素及总压畸变特征。
Characteristics and influence factors of total pressure distortion are studied based on tests conducted on a disturbed board installed in the nacelle inlet.
该软件利用综合畸变指数来描述进气畸变，实现了以往只有通过畸变试验才能进行的对进气畸变的研究。
It adopts distortion index to describe the inlet pressure distortion, which could only be studied through distortion experiments before.
介绍进气总压畸变对双轴涡喷发动机性能和稳定性影响的试验及其结果。
A brief view and results of tests for the effects of the inlet total pressure distortion on the performance and the stability of a two-spool turbojet engine are presented.
基于畸变进气下压气机实验特性，数值模拟了畸变进气下双轴涡喷发动机的总体性能。
Based on experimental properties of compressor under inlet distortion, the performance of twin-spool turbojet engines is studied in this paper by means of numerical simulation.
基于畸变进气下压气机实验特性，数值模拟了畸变进气下双轴涡喷发动机的总体性能。
Based on experimental properties of compressor under inlet distortion, the performance of twin-spool turbojet engines is studied in this paper by means of numerical simulation.
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