变截面悬臂翼板机械振动系统的复杂非线性动力学行为:实验与理论

IF 4.2 2区 工程技术 Q1 MECHANICS
Y.Z. Lian , W. Zhang , Y.H. Wang , Y. Wang , Y. Jiang
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引用次数: 0

摘要

对于飞机结构的非线性动力特性,通常采用理想模型来简化实际结构,以降低分析的复杂性并突出关键响应特性。通常将机翼建模为具有悬臂边界条件的变截面翼板,可以有效地研究结构在非线性振动中的主要特性。考虑石墨烯增强材料,采用实验和理论相结合的方法研究了变截面悬臂翼板的复杂非线性动力行为。系统在参数激励和横向激励下的非线性振动行为包括阈值面、共振响应、全局分岔和双参数多脉冲混沌运动。在进行理论研究之前,对悬臂变截面板进行了振动试验,结果证明了该机械振动系统存在复杂的动力行为。针对悬臂边界条件下变截面翼板的振动理论研究,考虑主共振、1/2次谐波参数共振和1:1内共振,采用多尺度摄动(MSP)方法得到了悬臂变截面翼板的平均方程。描述了幅频和力幅响应曲线,以检验共振响应。利用扩展Melnikov方法对系统在参数激励和横向激励下的阈值曲面、全局分岔和双参数多脉冲混沌动力学进行了计算。在同时共振的情况下,系统表现出经典的非线性硬弹簧特性和两个共振峰。在较大的参数激励或横向激励下,系统一阶模态的非线性行为变得更加明显,从而导致较大的共振峰。此外,系统中出现了多脉冲同斜轨道,导致系统在参数和横向联合激励下具有双参数多脉冲混沌振动特性。在参数激励和横向激励的影响下,系统出现周期和双参数多脉冲交替混沌运动。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Complex nonlinear dynamical behaviors of the mechanical vibration system for the cantilever wing plate with variable cross-section: Experiment and theory
For the nonlinear dynamic characteristics of aircraft structures, the idealized models are often used to simplify the actual structure to reduce the complexity of the analysis and highlight the key response characteristics. The wing is usually modeled as a variable-section wing plate with cantilever boundary conditions, which effectively studied primary structural behaviors in nonlinear vibration. Considering the graphene-reinforced materials, we investigate the complex nonlinear dynamic behaviors of the cantilever wing plate with variable cross-section by using the experiments and theory. The nonlinear vibrational behaviors include the threshold surface, resonance responses, global bifurcations and double-parameter multi-pulse chaotic motions for the system subjected to the parametric and transverse excitations. The vibrational test experiments for the cantilever variable cross section plate are conducted before the theoretical investigation, which the results certify the existence of the complex dynamical behaviors for the mechanical vibration system. For the vibrational theory study of the variable-section wing plate with cantilever boundary conditions, considering the primary resonances, 1/2 sub-harmonic parametric resonances, and the 1:1 internal resonance, the averaged equations for the cantilever variable cross section wing plate are obtained through the multiple scale perturbation (MSP) method. The amplitude-frequency and force-amplitude response curves are depicted to examine the resonant responses. The extended Melnikov method is utilized to evaluate the threshold surface, global bifurcations and double-parameter multi-pulse chaotic dynamics for the system subjected to the parametric and transverse excitations. In the case of the simultaneous resonances, the system exhibits the classical nonlinear hard spring characteristics and two resonance peaks. Under larger parametric or transverse excitations, the nonlinear behavior of the first-order modes for the system becomes more pronounced, resulting in larger resonance peaks. In addition, multi-pulse homoclinic orbits emerge in the system, leading to double-parameter multi-pulse chaotic vibration characteristics under combined the parametric and transverse excitations. Alternating periodic and double-parameter multi-pulse chaotic motions appear for the system in the influence of the parametric and transverse excitations.
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来源期刊
CiteScore
7.00
自引率
7.30%
发文量
275
审稿时长
48 days
期刊介绍: The European Journal of Mechanics endash; A/Solids continues to publish articles in English in all areas of Solid Mechanics from the physical and mathematical basis to materials engineering, technological applications and methods of modern computational mechanics, both pure and applied research.
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