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Part V: bifurcations of eigenvalues and stability problems in mechanics

机译:第五部分:力学中特征值和稳定性问题的分叉

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In this Part of the Lecture Notes we study bifurcations of eigenvalues of nonsymmetrical matrix operators depending on parameters with applications to the stability study in different mechanical problems. Section 1 gives general analysis of bifurcations for eigenvalues with geometric interpretation in two- and three-dimensional spaces. Main attention is focused on simple and double eigenvalues, and strong and weak interactions of eigenvalues are distinguished. In Section 2 stability and catastrophes in one-parameter circulatory systems with simple mechanical examples are studied. It is proven that in general they are subjected to catastrophes of three types: flutter, divergence, and transition from flutter to divergence and vice versa. In Section 3 properties of two-parameter circulatory systems are studied, and the explicit formulas describing metamorphoses of frequency curves are derived. These formulas use information on the system only at a merging point of the frequencies, and allow qualitative as well as quantitative analysis of behavior of frequency curves near that point with a change of parameters. In particular, development of "a bubble of instability" is analyzed. In Section 4 the Keldysh problem of aeroelastic stability of a wing with bracing struts is discussed, and the effect of disappearance of flutter instability revealed by Keldysh (1938) is explained. It is shown that this effect is connected with the convexity of the flutter domain in the parameter space. In Section 5 we study a problem of maximizing the critical buckling load of an elastic column of given length and volume assuming elastic supports at both ends of the column. This problem was first formulated by J.-L. Lagrange in 1773 for simply supported columns and has been considered by many authors for various boundary conditions. We obtain the bimodal optimal solutions and investigate their post-buckling behavior. Section 6 concerns instability domains for Hill's equation with damping under assumption of small excitation amplitude and damping coefficient. It is shown that these domains are halves of cones in the three-dimensional parameter space. One of the important applications of Hill's equation is connected with the stability study of periodic motions for nonlinear dynamical systems. It is shown how to find stable and unstable regimes for harmonically excited Duffing's equation.
机译:在这部分讲座中,我们根据应用于不同机械问题的稳定性研究的参数研究非对称矩阵运营商的特征值的分叉。第1节给出了在两维空间和三维空间中具有几何解释的特征值的分叉的一般性分析。主要注意力集中在简单和双峰等值上,特征值的强大和弱相互作用。在第2节中,研究了具有简单机械实施例的一参数循环系统中的稳定性和灾难。据证明,一般而言,它们受到三种类型的灾难:颤动,分歧和从颤动到发散的转变,反之亦然。在第3节中,研究了双参数循环系统的特性,得出了描述频率曲线变质的显式公式。这些公式仅在频率的合并点处使用关于系统的信息,并允许定性以及对参数附近的频率曲线附近的行为定量分析。特别地,分析了“不稳定的泡沫”的发展。在第4节中,讨论了具有支撑支撑的机翼的空气弹性稳定性的Keldysh问题,并解释了Keldysh(1938)揭示的颤动不稳定性的效果。结果表明,该效果与参数空间中的颤振域的凸起连接。在第5节中,我们研究了假设柱两端的弹性支撑的给定长度和体积的弹性柱的关键屈曲负荷的问题。这个问题首先由J.-1制定。 1773年Lagrange为简单支持的列,许多作者都考虑了各种边界条件。我们获得双峰最优解决方案并调查其后屈曲行为。第6节涉及山丘方程的不稳定域,在小激发幅度和阻尼系数的假设下阻尼。结果表明,这些畴是三维参数空间中的锥体的一半。 Hill等式的重要应用之一与非线性动力系统周期运动的稳定性研究相连。它显示了如何寻找稳定和不稳定的雄激动的Duffing等式的制度。

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