A gradient-based approach for optimal actuator design with morphing wings
Author:
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Control and Optimization,Mechanical Engineering,Aerospace Engineering,Civil and Structural Engineering,Software
Link
https://link.springer.com/content/pdf/10.1007/s11081-023-09835-7.pdf
Reference49 articles.
1. Achleitner J, Rohde-Brandenburger K, Rogalla von Bieberstein P, Sturm F, Hornung M (2019) Aerodynamic design of a morphing wing sailplane. In: AIAA Aviation 2019 Forum, American Institute of Aeronautics and Astronautics, Reston, Virginia. https://doi.org/10.2514/6.2019-2816
2. Arena M, Concilio A, Pecora R (2019) Aero-servo-elastic design of a morphing wing trailing edge system for enhanced cruise performance. Aerosp Sci Technol 86:215–235. https://doi.org/10.1016/j.ast.2019.01.020
3. Asins CC, Landersheim V, Laveuve D, Adachi S, May M, Wacker JD, Decker J (2021) Analysis and design of a leading edge with morphing capabilities for the wing of a regional aircraft–Gapless chord- and camber-increase for high-lift performance. Appl Sci 11(6):2752. https://doi.org/10.3390/app11062752
4. Baier HJ, Helwig G (1985) Integrated design and analysis approach for large precision structures. In: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. https://doi.org/10.2514/6.1985-805
5. Baier H, Datashvili L (2011) Active and morphing aerospace structures: a synthesis between advanced materials, structures and mechanisms. Int J Aeronaut Space Sci 12(3):225–240. https://doi.org/10.5139/ijass.2011.12.3.225
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