Aug 2026· Sound & Vibration· 0 citations· 34 references
Abstract
This study presents the structural and dynamic analysis of a real 60/15 flat-top tower crane with a free-standing height of 48 m. Finite element analyses were performed to evaluate the stress distribution, deformation, and dynamic characteristics of the main structural components. Based on the finite element results, a 17-degree-of-freedom (17-DOF) reduced-order mathematical model was developed. The stiffness coefficients were obtained from the finite element deformations using Hooke's law, while the damping coefficients were determined analytically. An elastic multibody model of the crane was also developed in MATLAB/SimMechanics to validate the proposed reduced-order model. The finite element analyses showed that the maximum equivalent stress remained below the allowable stress limit (approximately 225 MPa), while the maximum displacement of the mast reached 183.94 mm under the design loading condition. Modal analysis indicated that the counter-jib had the lowest first natural frequency (0.64 Hz), making it the most flexible structural component of the crane. Under the same 2-t tip load, the maximum difference between the proposed 17-DOF model and the SimMechanics model was only 4.86% in the jib tip deflection. These results show that the proposed model can accurately represent the structural behavior of the crane while providing a computationally efficient reduced-order representation of the crane compared with detailed finite element modeling. The developed model provides a practical tool for structural analysis, vibration evaluation, design studies, and future control applications of real flat-top tower crane systems.
A shell-element finite element model of the horizontal tail section of a civil aircraft iron bird test rig was developed in HyperMesh. Natural frequency extraction and modal effective mass fraction (MEFFMASS) analysis were performed using Nastran SOL 103, static strength assessment was carried out using SOL 101, and a...
Long-Wang Lei· Journal of Physics, Conferen...· 0 citations
A unified modeling framework is presented in this work to predict the free vibration and loss factor characteristics of damping sandwich rotational plates. The formulation starts from the first-order shear deformation theory, where the zigzag hypothesis and interlayer displacement continuity are combined to couple the...
<p>This paper presents a 2D nonlinear analysis of the load-carrying capacity of unbraced and concentrically braced steel frames subjected to lateral loading. The study was conducted using the incremental ("step-by-step") analytical method and finite element analysis. The effects of material and geometric nonlinearities...
Ivana Veličković, Milivoje Rogač· ASES CONGRESS 2026· 0 citations
The combined results demonstrate that implementing a one-way aero-structural coupling approach better predicts loading accuracy and the resultant structural response, giving a more reliable basis for preliminary aircraft wing design.
M. K. Abbas, T. Elsonni, Mokdad Hayawi Rahman et al.· Advances in Science and Tech...· 0 citations
The U-shaped stiffened plates are widely used in construction, machinery, ships and other fields. It will inevitably lead to structural vibration problems due to its various loads in engineering applications. The aim of this study is to establish a semi-analytical model for evaluating the vibration characteristics of U...
Cong Gao, Hong-Fu Wang, Shao-Wen Zhu et al.· International Journal of Str...· 0 citations
This technical note presents a practical numerical evaluation of the pull-out behavior of an embedded multi-plate PBL joint in a steel–concrete composite box girder, using the Hanjiang Bridge on the Xi’an–Shiyan High-Speed Railway as an engineering case. A three-dimensional nonlinear finite element model was establishe...
Yuan-Biao Gao, Long Chen, Xu-Hui Zhou et al.· Turkish Journal of Civil Eng...· 0 citations
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