In this paper, a new curvilinear method for correcting the gaseous compressibleeffect under higher subsonic and transonic intake condition upstream of the cascade is. presented.
文中还提出了压气机叶栅在高亚音速、跨音速工作条件下，修正气体压缩性影响的新的图线方法。
2
Effect of compressible term and that of viscous term are different in different time.
压缩项和粘性项的影响则随时间的不同而不同。
3
In this paper, the effect of compression does not be treated with PrandtI-Glauert's transformation, bat directly treated with compressible source (sink) and vortex.