Ismail, Mohd Shahrom, Nordin, Farhah Nadhirah, Le, Chi Hieu ORCID: 0000-0002-5168-2297 , Nguyen, Ho Quang and Mahmud, Jamaluddin (2024) The implementation of the single perturbation load approach to axially-compressed stiffened-stringer cylinder. In: Intelligent Manufacturing and Mechatronics: Selected Articles from iM3F 2023, 7th – 8th August, Pekan, Malaysia. Springer Proceedings in Materials (SPM) - iM3F: International conference on Innovative Manufacturing, Mechatronics & Materials Forum, 40 . Springer, Singapore, pp. 13-23. ISBN 978-9819998487; 978-9819998470 ISSN 2662-317X (Print), 2662-3161 (Online) (doi:https://doi.org/10.1007/978-981-99-9848-7_2)

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Abstract

This work study the influence of imperfections on axially compressed stiffened-stringer cylindrical shells for different geometries and materials that include aluminum and Carbon Fibre Reinforced Polymer (CFRP) using the finite element (FE) analysis. The imperfection technique called the single perturbation load approach (SPLA) is adopted. The verification analysis was performed with two cases reported in previous studies. Conversely, the parametric investigation was conducted focusing on the stiffener flange profile that varies its thickness and width. From the verification analyses SPLA demonstrated its attractive ability for designing imperfections in axially compressed aluminum stiffened cylindrical shells with fair agreement acquires. Finally, several design guidelines have been highlighted according to the parametric study and further deduced as imperfection sensitivity, buckling and post-buckling behaviour together with its collapse load and knockdown factor (KDF) of stringer stiffened cylindrical shells under axial compression primarily depend on the properties of shell and stiffeners themselves.

Item Type:	Conference Proceedings
Title of Proceedings:	Intelligent Manufacturing and Mechatronics: Selected Articles from iM3F 2023, 7th – 8th August, Pekan, Malaysia
Uncontrolled Keywords:	finite element analysis; stiffened-stringer cylindrical shell; knockdown factor; post-buckling; composite material; structural imperfection
Subjects:	T Technology > T Technology (General) T Technology > TA Engineering (General). Civil engineering (General) T Technology > TJ Mechanical engineering and machinery
Faculty / School / Research Centre / Research Group:	Faculty of Engineering & Science Faculty of Engineering & Science > School of Engineering (ENG)
Related URLs:	Publisher
Last Modified:	12 Apr 2024 14:15
URI:	http://gala.gre.ac.uk/id/eprint/46698

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