Influence mechanism of tip clearance on flutter stability with different aerodynamic coupling effects for transonic compressor
Jiali Xin,
Zongze He,
Xiaojing Lv
et al.
Abstract:Flutter is a highly destructive aeroelastic problem in modern compressors, which hinders the improvements of aero-engine performance and reliability. Because the aerodynamic work is mainly concentrated in the blade tip region, the tip clearance which is associated to the complex tip clearance flow has a considerable effect on the flutter stability. In this paper, in order to investigate the influence mechanism of the tip clearance on the flutter stability at different nodal diameters (ND), a series of compress… Show more
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