A Damage Tolerance Study of Curvilinearly Stiffened Panels with Different Crack Lengths Using a Global-local Finite Element Method-Reference-Cited by-同舟云学术

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A Damage Tolerance Study of Curvilinearly Stiffened Panels with Different Crack Lengths Using a Global-local Finite Element Method

Published:2013-04-05 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Islam Mohammad M.¹,Kapania Rakesh K.¹

Affiliation:

1. Virginia Polytechnic Institute and State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1475

Reference65 articles.

1. Future of Flight Vehicle Structures (2000 to 2023)

2. Design, Optimization, and Evaluation of Integrally Stiffened Al-7050 Panel with Curved Stiffeners

3. Optimal Design of Unitized Structures Using Response Surface Approaches

4. Vibro-Acoustic Optimization of Turbulent Boundary Layer Excited Panel with Curvilinear Stiffeners

Cited by 2 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. Global–Local Analysis of Composite Plate with Thin Notch;Journal of Aircraft;2014-05

2. EBF3PanelOpt: A Computational Design Environment for Panels Fabricated by Additive Manufacturing;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

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