Numerical simulations were carried out to investigate interaction between a singlestagecompressor and pylons.
采用数值模拟方法,对单级低速轴流压气机与发动机吊架之间的干涉进行了计算分析。
2
The hub treatment with a circumferential groove was tested on the stator hub and compared with the casing treatment over the rotor tip for a singlestage axial flow compressor.
在单级轴流压气机上,用周向槽式处理机匣在静子内径处进行轮毂处理,与转子尖部机匣处理作类比。
3
Experimental tests have been carried out to investigate the influence of inlet distortion on compressor stability margin in a low speed singlestage research compressor.