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Nonlinear dynamics of a two dimensional airfoil with freeplay in an inviscid compressible flow

机译:无粘性可压缩流动中具有自由游隙的二维翼型的非线性动力学

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摘要

A state space model for the aerodynamic loads calculated by means of a linearized CFD code which models the inviscid compressible flow is used to analyze the dynamic behavior of a two dimensional airfoil with a freeplay structural nonlinearity in pitch. The state space aeroelastic equations of motion are utilized to study the existence of Hopf bifurcation points and of limit cycle oscillations. Comparisons between the solutions of the coupled Euler-structural equations and the state space equations are provided.
机译:通过建模无粘性可压缩流的线性化CFD代码计算出的空气动力学载荷的状态空间模型,用于分析具有节距自由结构非线性的二维机翼的动力特性。利用状态空间气动弹性运动方程来研究Hopf分叉点和极限循环振荡的存在。给出了耦合的欧拉结构方程和状态空间方程解的比较。

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