智能 FG-GPLRC 夹层变厚截顶锥形壳体的非线性动态特性,前三阶模式的内部共振

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Shaowu Yang , Zhiquan Wang , Yuxin Hao , Wei Zhang , Yan Niu , Wensai Ma
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引用次数: 0

摘要

本文研究了在横向载荷和平面内力的共同作用下,简支变厚功能分级石墨烯平板增强复合材料(FG-GPLRC)智能截顶夹层锥壳的 1:1:1 内部共振非线性动力特性。截断式智能夹层锥形壳由一个不同厚度的 FG-GPLRC 核心层和两个磁电弹性面层组成,其材料属性和构成关系分别由混合规则、改进的 Halpin-Tsai 方法和广义胡克定律确定。利用一阶剪切变形理论(FSDT)、von Karman 几何非线性、汉密尔顿原理和 Galerkin 技术,建立了截顶智能 FG-GPLRC 锥壳的 3DOF 无量纲非线性动力学公式。应用多尺度技术建立了截顶智能 FG-GPLRC 锥壳在组合共振下的平均方程。非线性方程求解器和 Runge-Kutta 方法可以描绘出频率响应和力响应曲线、Poincare 图、相位图、时间历程图、分岔图和最大 Lyapunov 指数图。研究了阻尼和调谐参数、横向力和面内力对截断智能变厚 FG-GPLRC 夹层锥壳 1:1:1 内部共振非线性动态特性的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Nonlinear dynamic characteristics of smart FG-GPLRC sandwich varying thickness truncated conical shell with internal resonance for first three order modes
This paper examines the 1:1:1 internal resonant nonlinear dynamic characteristic of the simply supported varying thickness functionally graded graphene platelets reinforced composite (FG-GPLRC) smart truncated sandwich conical shell subject to the combined effects of transverse load and in-plane force. The truncated smart sandwich conical shell is composed of an FG-GPLRC varying thickness core and two magneto-electro-elastic face layers, whose material properties and constitutive relations are individually identified by the rule of mixture, improved Halpin-Tsai approach and generalized Hooke's law. Utilizing the first-order shear deformation theory (FSDT), von Karman's geometrical nonlinearity, Hamilton's principle and Galerkin technique, the 3DOF dimensionless nonlinear dynamic formulations for the truncated smart FG-GPLRC conical shell are established. The multiple-scale technique is applied to developing the averaged equations for the truncated smart FG-GPLRC conical shell under combined resonance. The frequency-response and force-response curves, Poincare maps, phase portraits, time history diagrams, bifurcation and maximum Lyapunov exponent diagrams can be portrayed by the nonlinear equation solver and Runge-Kutta approach. The effects of the damping and tuning parameters, transverse and in-plane forces on the 1:1:1 internal resonant nonlinear dynamic characteristic of truncated smart varying thickness FG-GPLRC sandwich conical shell are examined.
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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