Frequency Analysis of Ring-Stiffened Composite Cylindrical Shell using Experimental, Analytical and Finite Element Methods

ADMT Journal

دوره 16، شماره 2، شهریور 2023، صفحه 1-11   

نوع مقاله: Original Article

شناسه دیجیتال (DOI): 10.30486/admt.2021.1908459.1215

نویسندگان

Hadi Salimi¹؛ Ali Davar²؛ Mohsen Heydari Beni¹؛ Jafar Eskandari Jam^{* 2}؛ Majid Eskandari Shahraki³

¹Department of Mechanical Engineering, Malek Ashtar University of Technology, Tehran, Iran.

²Composite Research Centre, Malek Ashtar University of Technology, Lavizan, Tehran, Iran.

³Department of Aerospace Engineering, Ferdowsi University of Mashhad, Mashhad, Iran.

چکیده

In this paper, free vibration of laminated composite cylindrical shells reinforced with circumferential rings, are investigated with experimental, analytical and finite element methods and natural frequencies are obtained. The analysis is carried out for clamp-free and clamp-clamp boundary conditions and the results are compared with each other. To solve the problem, the equilibrium Equations of motions are written according to the classical shells theory and after simplification, the structural stiffness and mass matrices and the frequency Equation are derived using Galerkin method. The results obtained in this paper, are compared with the results available in the literatures, and the results of experimental and finite element methods and good agreement is observed.

کلیدواژه‌ها

Boundary Conditions؛ Composite Cylindrical Shells؛ Free Vibration؛ Galerkin Method؛ Reinforcement Rings

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