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声激励下绕二维薄翼非定常位势流的理论分析
引用本文:杨军,沙家正.声激励下绕二维薄翼非定常位势流的理论分析[J].空气动力学学报,1996,14(3):245-252.
作者姓名:杨军  沙家正
作者单位:南京大学
摘    要:本文根据无粘流体的非定常热流理论,推导出声源在亚声速不可压缩流场中对机翼产生的非定常流体动力的精确解,讨论了典型翼段上单极子声源的位置对声致气动载荷的影响,并通过对声-涡耦合的分析,解释了限于弱扰动的声激励消除颤振的机理,为有源声控制技术应用于流致振动和涡流的控制提供了理论基础。

关 键 词:机翼  声激励  非定常流  声-涡耦合  翼型

Theoretical Analysis of Unsteady Potential Flows Around Two-Dimensional Thin Airfoil Induced by Acoustic Excitations
Yang Jun, Sha Jiazheng, Qiu Xiaojun.Theoretical Analysis of Unsteady Potential Flows Around Two-Dimensional Thin Airfoil Induced by Acoustic Excitations[J].Acta Aerodynamica Sinica,1996,14(3):245-252.
Authors:Yang Jun  Sha Jiazheng  Qiu Xiaojun
Institution:Nanjing University
Abstract:In this paper,based on the unsteady potential theory of the inviscid fluid, the exact solutions of unsteady fluid dynamics induced by sound sorces in subsonic incompressible flows are derived, and the effects of the monopole sound sorce positions in the typical wing section on the acoustically induced aerodynamic loads are discussed. The analysis of the acoustic-vortex coupling explains the mechanism of the weak acoustic perturbation flutter surppression. It provides the theoretical foundation for the active acoustic control techniques applied to the control of fluidinduced vibration and vortex.
Keywords:acoustic excitations  unsteady flow  acoustic-vortex coupling    
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