4.7 Article

Post-buckling path and free vibration of a symmetric laminated plate vertically coupled with fluid under in-plane load

期刊

COMPOSITE STRUCTURES
卷 275, 期 -, 页码 -

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.compstruct.2021.114433

关键词

Laminated plate-fluid coupled system; Compressive in-plane load; Pre-and post-buckling state; Equilibrium path; Free vibration

资金

  1. National Natural Science Founda-tion of China [11702033, 52005047]
  2. Natural Science Basic Research Plan in Shaanxi Province of China [2020JQ-367, 2020JQ-345]
  3. China Postdoctoral Science Foundation [2021M692508, 2020M672129]

向作者/读者索取更多资源

This paper theoretically studies the effect of compressive in-plane load on the equilibrium paths and vibration characteristics of a vertical symmetric laminated plate coupled with fluid, in both pre-and post-buckling states. A two-step theoretical approach is developed, where nonlinear static equations are solved to trace snap-back behavior and stable buckling deflection, followed by calculation of coupled vibration characteristics using tangent stiffness. The number of limit points on the static unstable equilibrium path increases with larger compressive in-plane load in the post-buckling state, as shown by the theoretical and numerical results.
In this paper, the effect of compressive in-plane load on the equilibrium paths and vibration characteristics of a vertical symmetric laminated plate coupled with fluid is studied theoretically both in the pre-and post buckling state. The Third-order shear deformation theory and von Karman nonlinear strain displacement relationship are utilized to describe the nonlinear deformation of the plate consists of a number of fiber-reinforced layers. The Hamilton's principle is introduced to formulate the plate-fluid coupled governing equations. A twostep theoretical approach is developed. Firstly, based on the Cylindrical arc-length method, we solve the nonlinear static equations to trace the snap-back behavior and pass the limit points along the complex equilibrium paths obtaining the stable buckling deflection. Then the coupled vibration characteristics are calculated using the tangent stiffness at the stable positions. The present theoretical results are validated by the numerical results. The effects of added mass and hydrostatic load are compared and analyzed. It is noted that, in the post-buckling state, the number of limit points along the static unstable equilibrium path increases with the compressive in-plane load getting larger. The variation trends of the natural frequencies and modes under different in-plane loads in pre-and post-buckling state are investigated.

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