Influence of Fillers on the Post-buckling Behavior of the Hat-Stiffened Composite Panels
Author:
Funder
National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering
Link
https://link.springer.com/content/pdf/10.1007/s42405-023-00607-2.pdf
Reference28 articles.
1. Falzon BG, Faggiani A (2012) The use of a genetic algorithm to improve the postbuckling strength of stiffened composite panels susceptible to secondary instabilities. Compos Struct 94:883–895. https://doi.org/10.1016/j.compstruct.2011.10.015
2. Kumar NKC, Chavadaki S, Shaikh A (2020) Weight optimization of a hat stiffened panel of a typical transport aircraft composite wing. Mater Today Proc 26:471–547. https://doi.org/10.1016/j.matpr.2019.12.087
3. Soto A, González EV, Maimí P et al (2018) A methodology to simulate low velocity impact and compression after impact in large composite stiffened panels. Compos Struct 204:223–238. https://doi.org/10.1016/j.compstruct.2018.07.081
4. Mittelstedt C, Schroder KU (2010) Local postbuckling of hat-stringer-stiffened composite laminated plates under transverse compression. Compos Struct 92:2830–2844. https://doi.org/10.1016/j.compstruct.2010.04.009
5. Zhao L, Wang K, Ding F et al (2019) A post-buckling compressive failure analysis framework for composite stiffened panels considering intra-, inter-laminar damage and stiffener debonding. Res Phys 13:102205. https://doi.org/10.1016/j.rinp.2019.102205
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