Multi-Objective Optimization of Stiffened, Fiber-Reinforced Composite Fuselages for Mechanical and Vibro-Acoustic Requirements-Reference-Cited by-同舟云学术

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Multi-Objective Optimization of Stiffened, Fiber-Reinforced Composite Fuselages for Mechanical and Vibro-Acoustic Requirements

Published:2016-06-10 Issue: Volume: Page:
ISSN:
Container-title:17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
language:
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Author:

Serhat Gokhan¹,Faria Tiago Goncalves¹,Basdogan Ipek¹

Affiliation:

1. Koç University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3509

Reference31 articles.

1. MULTI-OBJECTIVE OPTIMIZATION OF ACOUSTIC SANDWICH PANELS

2. Multi-Disciplinary Design of Aircraft Fuselage Structures

3. Optimization of acoustic response

Cited by 5 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. Dynamic analysis of doubly curved composite panels using lamination parameters and spectral-Tchebychev method;Computers & Structures;2020-10

2. Unifying lamination parameters with spectral-Tchebychev method for variable-stiffness composite plate design;Composite Structures;2020-06

3. Multi-objective optimization of composite plates using lamination parameters;Materials & Design;2019-10

4. An investigation of the electromechanical coupling and broadband shunt damping in composite plates with integrated piezo-patches;Journal of Intelligent Material Systems and Structures;2019-09-15

5. Lamination Parameter Interpolation Method for Design of Manufacturable Variable-Stiffness Composite Panels;AIAA Journal;2019-07

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