The response of turbojet engine to the turbulence-type of dynamic inlettotalpressuredistortion is discussed in this paper.
本文介绍涡喷发动机对湍流型动态畸变的响应。
2
A stage - by - stage simulation method is introduced for analysis of inlettotalpressuredistortion 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。
3
A brief view and results of tests for the effects of the inlettotalpressuredistortion on the performance and the stability of a two-spool turbojet engine are presented.