航空学报 > 1995, Vol. 16 Issue (3): 2-7

计算振动翼面非定常气动力的Fourier级数展开法

刘千刚1, 刘群1, 吴凯1, 蔡喜源2   

  1. 1. 西北工业大学503 教研室, 西安, 710072;2. 机电部203 所, 陕西长安, 710111
  • 收稿日期:1993-08-06 修回日期:1994-03-25 出版日期:1995-06-25 发布日期:1995-06-25

A FOURIER SERIES EXPANSION METHOD FOR CALCULATING THE UNSTEADY AERODYNAMIC LOADS ON OSCILLATING WINGS

Liu Qiangang1, Liu Qun1, Wu Kai1   

  1. 1. Faculty 503, Northwestern Polytechnical University, Xi'an, 710072;2. 203rd Institute, Ministry of Electronics and Machinery, Changan, Shaanxi, 710111
  • Received:1993-08-06 Revised:1994-03-25 Online:1995-06-25 Published:1995-06-25

摘要: 将翼面绕基准状态作任意形态的振动,用Fourier级数展为n个不同振幅、不同频率的谐波;用Green函数法计算每个谐波引起的非定常气动力;然后在时域中将它们叠加,即可求得该翼面在时域中以给定的波形作振动时的非定常气动力。重点讨论了翼面作接近方波形振动时的非定常气动力。算例表明,该方法所得结果与其他方法及实验结果吻合。

关键词: 傅里叶级数, 非定常空气动力学, 格林函数, 数值分析

Abstract: The arbitrary vibration motion of a wing around its reference state is expanded into Fourier series of n harmonic waves with different amplitudes and frequencies. The unsteady aerodynamic load due to each harmonic motion is calculated by the Green′s function method; by superposing them in the time domain. The unsteady aerodynamic loads of the given vibration motion are obtained. Much discussion is given on the unsteady aerodynamic loads caused by approximately square waves motion. Numerical examples show that the results of the present method are in good agreement with the results of other methods and experimental data.

Key words: Four ier series, unsteady aerodynamics, Greencs function, numerical analysis

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