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静子尾迹对转子叶片气弹稳定性的影响

Translated title of the contribution: Influence of stator wake on aeroelasticity of rotor blade
  • Beihang University
  • Collaborative Innovation Center for Advanced Aero-Engine

Research output: Contribution to journalArticlepeer-review

Abstract

An energy method was proposed to consider the effect of the wake induced by the upstream stator on the aeroelasticity of the rotor blade based on the phase lagged method, and then validated by the time-marching method. The effects of wake on aerodynamic damping of rotor blades under different modes and interblade phase angles were investigated. The results showed that the wake had a significant effect on the aeroelasticity of the rotor blades, and can be simulated by the developed method accurately and efficiently. Compared with the first torsional mode, the wake had a more serious impact on the aeroelasticity of the first bending mode. Furthermore, for different interblade phase angles, the wake can weaken the low aerodynamic damping and strengthen the high damping for the first bending mode, in contrast to the first torsion mode.

Translated title of the contributionInfluence of stator wake on aeroelasticity of rotor blade
Original languageChinese (Traditional)
Pages (from-to)2219-2227
Number of pages9
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume33
Issue number9
DOIs
StatePublished - 1 Sep 2018

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