An interlaminar damage shell model for typical composite structures-Reference-Cited by-同舟云学术

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An interlaminar damage shell model for typical composite structures

Published:2024-01 Issue:1 Volume:37 Page:118-137
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

ZHOU Jie,WU Zhen,LIU Zhengliang,REN Xiaohui

Funder

National Natural Science Foundation of China

Natural Science Foundation of Shaanxi Province

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference54 articles.

1. A review on plate and shell theories for laminated and sandwich structures highlighting the Finite Element Method;Caliri;Compos Struct,2016

2. Another approach to linear shell theory and a new proof of Korn’s inequality on a surface;Ciarlet;Comptes Rendus Math,2005

3. A refined element-based Lagrangian shell element for geometrically nonlinear analysis of shell structures;Jung;Adv Mech Eng,2015

4. Free vibration analysis of laminated plate/shell structures based on FSDT with a stabilized nodal-integrated quadrilateral element;Nguyen-Van;J Sound Vib,2008

5. Classical, higher-order, zig-zag and variable kinematic shell elements for the analysis of composite multilayered structures;Carrera;Eur J Mech A/solids,2018

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Nonlinear dynamic modeling and experimental study of full-composite cylindrical shells with a foam-filled cavity lattice core;Nonlinear Dynamics;2023-10-03

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