An improved streamline curvature numerical method is modified and applied to better approximate the flow fields of multi-stage transonic axialcompressors.
本文采用改进的流线曲率法对跨声速多级轴流压气机非设计点进行了性能模拟。
2
An improved streamline curvature numerical method is modified and applied to better approximate the flow fields of multi-stage transonic axialcompressors.
本文采用改进的流线曲率法+对跨声速多级轴流压气机非设计点进行了性能模拟。
3
In comparison with the axial turbomachinery, the internal flow in centrifugal compressors is more complex.