A new three-dimensional aerodynamic stability model for an axial flowcompressor to study the effects of radial disturbance on the rotating stall is presented.
给出了考虑压气机径向扰动对失速影响的轴流压气机三维气动稳定性模型。
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The result shows that the boundary layer radial vortex becomes an important factor for causing compressorflow instability.