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Frequency-domain identification of time-varying systems for analysis and prediction of aeroelastic flutter

机译:时变系统的频域识别,用于气动弹性颤振的分析和预测

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In this paper a different approach to wind tunnel flutter testing is presented. This procedure can now be performed as one continuous test, resulting in a major time saving. Both analysis of the current behaviour of the structure, and prediction towards higher velocities, are important for flight flutter testing, and are dealt with in this paper. The recently developed time-varying weighted non-linear least-squares estimator (TV-WNLS) (Lataire and Pintelon, 2011 ) is applied to the aeroelastic flutter problem. Smooth variation of the transfer function coefficients is forced through the TV-WNLS estimator, and the obtained polynomials are used as basis for predicting the damping ratio towards higher velocities. Selection of the model order is based on linear variation of the airspeed and the evaluation of Theodorsen's unsteady aerodynamics for the frozen time-varying aeroelastic system at a certain constant velocity. Therefore, providing a physical justification for the extrapolation of the damping ratio towards higher velocities. The method is applied to wind-tunnel measurements on a cantilevered wing. It is shown that the proposed method outperforms flutter speed prediction by classic damping ratio extrapolation and a non-parametric analysis of the time-varying signal.
机译:本文提出了一种不同的风洞颤振测试方法。现在可以将该过程作为一项连续测试执行,从而节省了大量时间。对结构当前行为的分析以及对更高速度的预测都对飞行颤振测试很重要,本文将对此进行讨论。最近开发的时变加权非线性最小二乘估计器(TV-WNLS)(Lataire和Pintelon,2011年)被应用于气动弹性颤振问题。通过TV-WNLS估计器强制传递函数系数的平滑变化,并且将获得的多项式用作预测朝向更高速度的阻尼比的基础。模型顺序的选择是基于空速的线性变化以及在一定的恒定速度下对冷冻时变气动弹性系统的Theodorsen非定常空气动力学的评估。因此,为将阻尼比外推到更高的速度提供了物理依据。该方法适用于悬臂机翼的风洞测量。结果表明,通过经典的阻尼比外推和时变信号的非参数分析,该方法优于颤振速度的预测。

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