the unsteady surface pressure on stator blade of an axial compressor was measured by means of mounting micro-sensors on blades surface.
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 stator blade flange extends away from each blade such that the secondary leading edge points generally to the primary leading edge of a preceding stator blade.
该导轮叶片凸缘从每个叶片延伸出,从而使得次前缘通常指向前一导轮叶片的主前缘。
an experimental study of the stator blade wake in a small axial compressor is performed by using a hotwire anemometer (hwa) under different rotating speeds and mass flow conditions.