Mixed Finite-Element Analysis of Thick Doubly Curved Laminated Shells-Reference-Cited by-同舟云学术

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Mixed Finite-Element Analysis of Thick Doubly Curved Laminated Shells

Published:1995-01 Issue:1 Volume:8 Page:43-53
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:Journal of Aerospace Engineering

Author:

Wu Chih-Ping,Liu Chi-Chuan

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290893-1321%281995%298%3A1%2843%29

Reference23 articles.

1. Exact Elasticity Solution for Laminated Anisotropic Cylindrical Shells

2. An approximate method for prediction of transverse shear stresses in a laminated shell

3. Analysis of Laminated Shells of Revolution

4. Analytical Solutions for Thick, Doubly Curved, Laminated Shells

5. A survey of finite element models for the analysis of moderately thick shells

Cited by 10 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. A new bending model for composite laminated shells based on the refined zigzag theory;Archive of Applied Mechanics;2022-07-15

2. Modeling of cylindrical composite shell structures based on the Reissner’s Mixed Variational Theorem with a variable separation method;Advanced Modeling and Simulation in Engineering Sciences;2019-05-18

3. C0 Layerwise Model with Fixed Degrees of Freedom and Variable In- and Out-of-Plane Kinematics by Strain Energy Updating Technique;Aerospace;2015-11-17

4. Development of an Efficient Zigzag Model with Variable Representation of Displacements across the Thickness;Journal of Engineering Mechanics;2014-03

5. Extension of the Strain Energy Updating Technique to a Multilayered Shell Model with Adaptive Displacements and Fixed DOF;Journal of Aerospace Engineering;2013-10

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