Local optimisation of long anisotropic laminated fibre composite panels with T shape stiffeners-Reference-Cited by-同舟云学术

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Local optimisation of long anisotropic laminated fibre composite panels with T shape stiffeners

Published:2006-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th
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Author:

Herencia J.,Weaver Paul,Friswell Michael

Publisher

American Institute of Aeronautics and Astronautics

Reference34 articles.

1. 3Jones, R. M."Mechanics ofcompositematerials". 2ndedition.Taylor andFrancis,Inc.,325 Chestnutstreet,Philadelphia,PA19106. pp.26-31.1999.

2. Analysis of Anisotropic Plates

3. Importance of anisotropy on buckling of compression-loaded symmetriccomposite plates

Cited by 4 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. Structural Optimization of Composite Panel with Lamination Parameters and Equivalent Stiffness Laminate Method;Applied Mechanics and Materials;2014-01

2. A lamination parameter-based strategy for solving an integer-continuous problem arising in composite optimization;Computers & Structures;2013-11

3. Ply number rounding-off in optimization of composite structures using lamination parameters;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23

4. Optimum Buckling Design for Composite Wing Cover Panels with Manufacturing Constraints;48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2007-04-23

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