Geometrically Nonlinear Coupled-Adjoint Aerostructural Optimization of Ultra-High Aspect Ratio Wings with Flutter Constraints-Reference-Cited by-同舟云学术

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Geometrically Nonlinear Coupled-Adjoint Aerostructural Optimization of Ultra-High Aspect Ratio Wings with Flutter Constraints

Published:2023-01-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2023 Forum
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Author:

Ma Yiyuan¹,Abouhamzeh Morteza¹,Da Ronch Andrea²,Elham Ali²

Affiliation:

1. Technische Universitat Braunschweig

2. University of Southampton

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2023-2205

Reference32 articles.

1. Conceptual design and comparative study of strut-braced wing and twin-fuselage aircraft configurations with ultra-high aspect ratio wings

2. Design Optimization of a Truss-Braced-Wing Transonic Transport Aircraft

3. Tradeoffs of Wing Weight and Lift/Drag in Design of Medium-Range Transport Aircraft

Cited by 1 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. Designing high aspect ratio wings: A review of concepts and approaches;Progress in Aerospace Sciences;2024-02

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