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Method determining the nature of oscillating motion of the aircraft based on the analysis of coefficients of aerodynamic damping derivatives

机译:基于空气动力学阻尼导数系数分析的确定飞机振荡运动性质的方法

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摘要

Analysis of experimental data shows that the nature of the oscillating motion of an aircraft does not depend uniquely on the value of the coefficients of aerodynamic damping derivatives. The present work makes an attempt to explain this phenomenon and develops a methodology to adequately characterize the oscillating motion of aircraft based on the analysis of the coefficients of aerodynamic damping derivatives.
机译:对实验数据的分析表明,飞机的振荡运动的性质并不唯一地取决于空气动力学阻尼导数的系数值。本工作试图解释这种现象,并基于对空气动力学阻尼导数系数的分析,开发出一种方法来充分表征飞机的振荡运动。

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