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Author:

Shao, D. (Shao, D..) | Zhang, Y. (Zhang, Y..) | Cao, Y. (Cao, Y..) | Tao, Y. (Tao, Y..) | Zhao, Y. (Zhao, Y..)

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Scopus SCIE

Abstract:

A general modeling approach is presented to analyze the free vibration behavior of the spatially coupled shell-plate system (SCSPS) with complex geometric shapes. The coupling mechanism established by the penalty function method can be applied not only to the SCSPS but also to other extensively studied shell-plate structures. The conventional method for irregularly-shaped plates involves the utilization of one-to-one mapping technology (OTOMT) to transform the two-dimensional plane domain of the plate into a square domain, aiming to fulfill the numerical solution requirement for integral calculation. However, since the OTOMT is a planar mapping technique that cannot be applied to shells, in this paper, we propose a coordinate transformation strategy to convert two-dimensional shells into plane geometry in order to address this limitation. The vibration problem is simultaneously resolved numerically using the Hamilton's principle and the Jacobi spectral method. The current method is validated for several key capabilities based on three case studies, as well as modal experiments and the commercial finite element software. Additionally, a series of model evaluations are employed to demonstrate the advantages of the current method. Moreover, the results of the parametric study illustrate the impact of several variables on the natural frequency of the structure. © 2024 Elsevier Ltd

Keyword:

Coordinate transformation Spatially coupled shell-plate system with complex geometric shapes Free vibration Jacobi spectral method Modal experiments

Author Community:

  • [ 1 ] [Shao D.]College of Mechanical & Energy Engineering, Beijing University of Technology, Beijing, 100124, China
  • [ 2 ] [Zhang Y.]College of Mechanical & Energy Engineering, Beijing University of Technology, Beijing, 100124, China
  • [ 3 ] [Zhang Y.]AVIC Beijing Keeven Aviation Instrument Co., Ltd., Aviation Industry Corporation of China, Ltd, Beijing, 101300, China
  • [ 4 ] [Cao Y.]Naval Research Institute, Beijing, 100161, China
  • [ 5 ] [Tao Y.]Beijing Aerospace Technology Institute, China Aerospace Science & Industry Corp., Beijing, 100074, China
  • [ 6 ] [Zhao Y.]College of Mechanical & Energy Engineering, Beijing University of Technology, Beijing, 100124, China

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Source :

Engineering Analysis with Boundary Elements

ISSN: 0955-7997

Year: 2024

Volume: 167

3 . 3 0 0

JCR@2022

Cited Count:

WoS CC Cited Count:

SCOPUS Cited Count:

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 7

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