Improving the Airplane Efficiency by Use of Wing Maneuver Load Alleviation
Author:
Affiliation:
1. Aerophysics Research Corporation, Bellevue, Wash.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.59169
Reference5 articles.
Cited by 20 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. Fluid–Structure Coupled Analysis of Maneuver Load Alleviation on a Large Transport Aircraft;Journal of Aircraft;2024-07
2. Fluid-Structure Coupled Analysis of Maneuver Load Alleviation on a Large Transport Aircraft;AIAA AVIATION 2023 Forum;2023-06-08
3. Bi-level Multidisciplinary Design Optimization of a Wing Considering Maneuver Load Alleviation and Flutter;AIAA SCITECH 2023 Forum;2023-01-19
4. Load Alleviation of Flexible Aircraft by Dynamic Control Allocation;Journal of Guidance, Control, and Dynamics;2022-10
5. Global aero-structural design optimization of composite wings with active manoeuvre load alleviation;CEAS Aeronautical Journal;2022-05-25
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