Postbuckling of Stiffened Panels Using Strut, Strip, and Finite Element Methods
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2061
Reference16 articles.
1. Finite strip post-local-buckling analysis of composite prismatic plate structures
2. PANDA2—Program for minimum weight design of stiffened, composite, locally buckled panels
3. Optimum design using viconopt, a buckling and strength constraint program for prismatic assemblies of anisotropic plates
4. Analysis and Testing of a Postbuckled Stiffened Panel
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. Design rules for stiffened panel buckling containment features;Thin-Walled Structures;2017-07
2. Exact strip analysis and optimum design of aerospace structures;The Aeronautical Journal;2010-08
3. Postbuckling of Composite Stiffened Panels Using Exact Strip Analysis with Newton Iteration;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07
4. Optimization of Postbuckled Stiffened Panels with Multiple Stiffener Sizes;48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2007-04-23
5. Bilevel Optimization and Postbuckling of Highly Strained Composite Stiffened Panels;AIAA Journal;2006-11
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