Investigations Into the Stability of Thin-Walled Composite Structures with Top-Hat Cross-Sections
Author:
Affiliation:
1. 1 Faculty of Mechanical Engineering, Department of Machine Design and Mechatronics , Lublin University of Technology , ul. Nadbystrzycka 38D, 20-618 Lublin , Poland
Abstract
Publisher
Walter de Gruyter GmbH
Subject
Mechanical Engineering,Control and Systems Engineering
Link
https://www.sciendo.com/pdf/10.2478/ama-2023-0036
Reference25 articles.
1. Barkanov E, Ozoliņš O, Eglītis E, Almeida F, Bowering MC, Watson G. Optimal design of composite lateral wing upper covers. Part I: Linear buckling analysis, Aerospace Science and Technology. 2014;38: 1-8. https://doi.org/10.1016/j.ast.2014.07.010
2. Orifici AC, Thomson RS, Degenhardt R, Kling A, Rohwer K, Bayandor J. Degradation investigation in a postbuckling composite stiffened fuselage panel. Composite Structures. 2008;82(2): 217-224 https://doi.org/10.1016/j.compstruct.2007.01.012
3. Bambach MR. Fibre composite strengthening of thin-walled steel vehicle crush tubes for frontal collision energy absorption. Thin-Walled Structures. 2013;66: 15-22. https://doi.org/10.1016/j.tws.2013.02.006
4. Hutchinson JW, Koiter WT. Postbuckling theory. Applied Mechanics Reviews. 1970;12: 1353-1366.
5. Byskov E, Hutchinson JW. Mode interaction in axially stiffened cylindrical shells. AIAA. 1977;15(7):941-948. https://doi.org/10.2514/3.7388
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