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Active Aeroelastic Control over a Multi- Surface Wing: Modelling and Wind Tunnel Testing

机译：多表面机翼的主动气动弹性控制：建模和风洞测试

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《AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference》|2007年|P.1-16|共16页
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A. De;
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中图分类航空器结构力学;
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1. Active Aeroelastic Control Over a Multisurface Wing: Modeling and Wind-Tunnel Testing [J] . A. De Gaspari, S. Ricci, L. Riccobene, AIAA Journal . 2009,第9期

机译：多翼机翼的主动气动弹性控制：建模和风洞测试
2. Control Surface Response of a Blended Wing Body Aeroelastic Wind-Tunnel Model [J] . Martin Carlsson Journal of Aircraft . 2005,第3期

机译：机翼混合气弹风洞模型的控制表面响应
3. Design of aeroelasticity bench test for NACA0012 wing model in the low speed wind tunnel: Influence of wing's parameters on flutter speed [J] . Thi Tuyet Nhung Le, Chi-Cong Nguyen, Hoang Nam Vang International Journal of Mechanical Engineering and Applications . 2015,第1a3期

机译：低速风洞中NACA0012机翼模型的空气弹性台架试验设计：机翼参数对扑扑速度的影响
4. Active Aeroelastic Control over a Multi- Surface Wing: Modelling and Wind Tunnel Testing [C] . American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/American Society of Civil Engineers/Vertical Flight Technical Society/ASC Structures, Structural Dynamics, and Materials Conference . 2007

机译：多表面翼的主动空气控制：建模和风洞测试
5. Development of an Active Aeroelastic Continuous Trailing Edge Wind Tunnel Wing Model for Drag and Gust Load Minimization [D] . Mundt, Tyler. 2019

机译：开发积极的空气弹性连续后缘风隧道翼模型，用于阻力和阵风负荷最小化
6. Fuzzy Logic-Based Control for a Morphing Wing Tip Actuation System: Design Numerical Simulation and Wind Tunnel Experimental Testing [O] . Shehryar Khan, Teodor Lucian Grigorie, Ruxandra Mihaela Botez, 2019

机译：变形翼尖驱动系统的基于模糊逻辑的控制：设计数值模拟和风洞实验测试
7. Control Surface Interaction Effects of the Active Aeroelastic Wing Wind Tunnel Model [O] . Heeg Jennifer 2006

机译：主动气动弹性翼风洞模型的控制面相互作用效应
8. Control Surface Interaction Effects of the Active Aeroelastic Wing Wind Tunnel Model [R] . Heeg, Jennifer 2006

机译：主动气动弹性翼风洞模型的控制面相互作用效应

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