Preliminary weight estimation of conventional and joined wings usingequivalent beam models
Author:
Affiliation:
1. University of Florida, Gainesville, Florida
2. National Cheng Kung University, Taiwan, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45625
Reference5 articles.
Cited by 18 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. Physics-Based Lifting Surface Weight Estimation for Conceptual Design of Vertical Takeoff and Landing Aircraft;AIAA AVIATION 2023 Forum;2023-06-08
2. Structural Analysis and Optimization of Wings Subjected to Dynamic Loads;AIAA Journal;2022-02
3. Aeroelastic Optimization Design of the Global Stiffness for a Joined Wing Aircraft;Applied Sciences;2021-12-12
4. An Efficient Method to Dimensionally Reduce Aperiodic Inhomogeneous 3-D Structures to 1-D Beam-Like Structures;AIAA Scitech 2020 Forum;2020-01-05
5. Beam Theory for Asymptotic Analysis of Aperiodic and Inhomogeneous Structures;AIAA Journal;2019-10
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