rotating inlet distortion 旋转进气畸变
total pressure inlet distortion 总压进口畸变
inlet total temperature distortion 进气总温畸变
inlet dynamic distortion 进气道动态畸变
inlet swirl flow distortion 进气旋流畸变
inlet total pressure distortion 进气总压畸变
inlet flow distortion 进口流场畸变
inlet pressure distortion 进气压力畸变
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。
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。
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。
应用推荐