Iranian Journal of Mechanical Engineering Transactions of ISME

Iranian Journal of Mechanical Engineering Transactions of ISME

Finite Element Analysis of Longitudinal and Transverse Semi-elliptical Cracks in Composite CNG Cylindrical Tanks with Metal Lining under Internal Pressure and Thermal Loading

Authors
1 Assistant Professor, Department of Mechanical Engineering, Technical and Engineering Faculty, University of Qom, Qom, Iran
2 MSc Graduated Student, Department of Mechanical Engineering, Technical and Engineering Faculty, University of Qom, Qom, Iran
Abstract
Crack formation and propagation is one of the important factors in the failure of engineering components, which can cause great financial and human losses. Therefore, it is very necessary to investigate and study the cracks in structures under load. In this paper, a semi-elliptical crack in composite CNG pressure tanks with a metal liner is investigated. The tank under study is a type III CNG pressure tank. In this tank, whose composite coating is made of Boron/epoxy, Kevlar/epoxy, and carbon/epoxy; longitudinal and transverse internal cracks as well as external cracks have been investigated. The results show that the crack geometry has a great influence on the stress intensity factor. The internal longitudinal semi-elliptical crack is the most critical crack and when this crack is located next to the external transverse crack, it becomes more critical and the stress intensity factor in the internal longitudinal semi-elliptical crack increases. The Boron/epoxy composite has a greater resistance to increased internal pressure and increasing the number of composite layers increases the crack stress intensity factor. Also, in a tank with Boron/epoxy coating, an angle of 40 to 45 degrees to the longitudinal and transverse cracks is the best position for fiber placement. If this angle is greater or less, the stress intensity factor increases.
Keywords

Subjects


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  • Receive Date 26 February 2025
  • Revise Date 03 May 2025
  • Accept Date 03 June 2025