Nonlinear Aeroelastic Effects in Flapping Wing Micro Air Vehicles

Author:

Gogulapati Abhijit,Friedmann Peretz,Shyy Wei

Publisher

American Institute of Aeronautics and Astronautics

Cited by 7 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. A modified unsteady-nonlinear aeroelastic model for flapping wings;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-06-14

2. Analytical structural behaviour of elastic flapping wings under the actuator effect;The Aeronautical Journal;2018-07-04

3. Approximate Aeroelastic Modeling of Flapping Wings in Hover;AIAA Journal;2013-03

4. Measurements of the Aerodynamic Characteristics of Low Aspect Ratio Wings in Complex Motions;41st AIAA Fluid Dynamics Conference and Exhibit;2011-06-14

5. Flight Dynamic Stability of a Flapping Wing Micro Air Vehicle in Hover;52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2011-04-04

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