4.6 Article

Deformation Performance Analysis of a Truss Structure Based on the Deformation Decomposition Method

Journal

BUILDINGS
Volume 12, Issue 3, Pages -

Publisher

MDPI
DOI: 10.3390/buildings12030258

Keywords

plane truss structure; deformation decomposition; countable mode shapes; quantitative analysis; tension and compression deformation

Funding

  1. National Natural Science Foundation of China [51878621]
  2. Key Research Projects of Henan Higher Education Institutions [22A560005]

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This paper proposes a method for comprehensive deformation analysis of a truss and verifies its correctness and superiority by comparing it with traditional methods. Additionally, a relative deformation decomposition method is introduced for detailed analysis. Furthermore, the method is applied to analyze the relative deformation of a plane truss structure under different load conditions. The basic deformation performance of the structure can be quantitatively analyzed using countable mode shapes.
Trusses are among the basic components of large-span bridges and large-space structures. A method is proposed to conduct a comprehensive deformation analysis of a truss in terms of the basic rigid body displacements and the tension and compression deformation based on complete mathematical orthogonality and mechanical equilibrium. The correctness of the proposed method is verified by comparison with a traditional strain analysis. Furthermore, a relative deformation decomposition of the mode shape is proposed to analyse in detail its relative displacement and deformation. The correctness and superiority of the proposed method are verified by comparison with the modal mass participation coefficient method and the animation from observation method. Additionally, the relative deformation decomposition of a plane truss structure is realized under any load conditions based on the superposition of mode shapes. The quantitative analysis of the basic deformation performance of a plane truss structure can also be conducted by countable mode shapes, which do not involve load conditions. Finally, the number of mode shapes that must be considered differs when using the maximum displacement and the tension and compression deformation analysis indicators.

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