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卡门涡街与翼型的相互作用
引用本文:朱克勤.卡门涡街与翼型的相互作用[J].空气动力学学报,1992,10(4):422-434.
作者姓名:朱克勤
作者单位:中国科学技术大学 (朱克勤),马克斯·普朗克流体力学研究所(Obermeier F.)
摘    要:本文利用保角变换,用离散涡方法求解了卡门涡街与翼型的相互作用。较详细地分析了它作为偶极子声源的特性,并模拟了在涡翼相互作用过程中尾迹的发生和演化。计算结果表明:在相互作用时,尾迹所吸收的声能可以是正值也可以是负值;升力和声偶极子强度出现了周期性脉动,这种脉动与翼型的振动和噪声有直接的关系。

关 键 词:涡翼干扰  离散涡法  涡声  涡街

KARMAN VORTEX STREET-AIRFOIL INTERACTION
Zhu Keqin.KARMAN VORTEX STREET-AIRFOIL INTERACTION[J].Acta Aerodynamica Sinica,1992,10(4):422-434.
Authors:Zhu Keqin
Abstract:. Based on the discrete vortex method, a conformal mapping technique is used to solve Karman vortex street-airfoil interaction. The characteristics of the interaction as an acoustic source of dipole type arc investigated and the evolution of the wake is simulated. Calculating results show that the sound power absorbed by the wake may be positive or negative during the time process. It is also found that the strength of acoustic dipole in the far field and airfoil lift appear periodic fluctuation. This kind of periodic fluctuation is one of the main reasons, which is responsible for the aerodynamic noise and for the oscillation of airfoils.
Keywords:vortex-airfoil interaction  discrete vortex method  vortex sound  vortex street  
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