Optimization of Postbuckled Stiffened Panels with Multiple Stiffener Sizes-Reference-Cited by-同舟云学术

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Optimization of Postbuckled Stiffened Panels with Multiple Stiffener Sizes

Published:2007-04-23 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Watson Andrew¹,Featherston Carol²,Kennedy David²

Affiliation:

1. Loughborough University

2. Cardiff University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-2207

Reference15 articles.

1. Optimum Design of Stiffened Panels With Substiffeners

2. Optimization of composite, stiffened, imperfect panels under combined loads for service in the postbuckling regime

3. Design of panels having postbuckling strength

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1. Topology optimization for stiffened panels, from linear buckling to postbuckling;AIAA SCITECH 2023 Forum;2023-01-19

2. Design charts for the local buckling analysis of integrally web-stiffened panels with filleted junctions subjected to uniaxial compressive loads;Thin-Walled Structures;2022-02

3. Uçak Kanadının Entegre Güçlendirilmiş Panel Yapıları Kullanılarak Yapısal Tasarımı;European Journal of Science and Technology;2020-04-30

4. Wing Panel Design with Novel Skin-Buckling Containment Features;Journal of Aircraft;2016-03

5. Hybrid analysis and optimization of hierarchical stiffened plates based on asymptotic homogenization method;Composite Structures;2015-11

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