Levy-Type Boundary Fourier Analysis of Thick Cross-Ply Panels with Negative Gaussian Curvature-Reference-Cited by-同舟云学术

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Levy-Type Boundary Fourier Analysis of Thick Cross-Ply Panels with Negative Gaussian Curvature

Published:2015-09 Issue:9 Volume:53 Page:2492-2503
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Chaudhuri Reaz A.¹,Oktem Ahmet Sinan²,Guedes Soares C.³

Affiliation:

1. Department of Materials Science and Engineering, University of Utah, Salt Lake City, Utah 84112-0560

2. Department of Mechanical Engineering, Gebze Technical University, 41400 Kocaeli, Turkey

3. Centre for Marine Technology and Engineering, University of Lisbon, 1049-001 Lisbon, Portugal

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053440

Reference46 articles.

1. Stability of thin shallow shells of negative Gaussian curvature

2. A finite element formulation for shells of negative Gaussian curvature

3. Arbitrarily laminated, anisotropic cylindrical shell under internal pressure

4. Admissible boundary conditions and solutions to internally pressurized thin arbitrarily laminated cylindrical shell boundary-value problems

5. Internally Pressurized Thin Unsymmetric Cross-Ply Cantilever Cylindrical Shells

Cited by 6 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. Flattening Effect of Negative Gaussian Curvature on Simply Supported Thick Asymmetric Cross-Ply Panels in the Absence of Surface-Parallel Edge Restraints;Journal of Aerospace Engineering;2020-11

2. Modeling and analysis of cross-ply and angle-ply laminated plates under patch loads using RBF based meshfree method and new HSDT;Computers & Mathematics with Applications;2020-04

3. Geometrically nonlinear analysis of FG doubly-curved and hyperbolical shells via laminated by new element;STEEL COMPOS STRUCT;2018

4. Bending performance of laminated sandwich shells in hyperbolic paraboloidal form;STEEL COMPOS STRUCT;2017

5. Simply-Supported Saddle-Shaped Thick Symmetric Cross-Ply Panels: Full Surface-Parallel Boundary Constraints;AIAA Journal;2016-07

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