Longitudinal Aerodynamics of Rapidly Pitching Fixed-Wing Micro Air Vehicles

Author:

Randall Ryan,Shkarayev Sergey,Abate Gregg,Babcock Judson

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference22 articles.

1. Hoffman, C. "Design, Construction, and Study of Flight Dynamics of Fixed-Wing MAV with Hovering Capabilities," Master of Science Thesis,Dept. of Aerospace Engineering, Bundeswehr Univ., Munich,2008.

2. Aerodynamic Design of Micro Air Vehicles for Vertical Flight

3. Experiments in Fixed-Wing UAV Perching

4. Longitudinal Dynamics of a Perching Aircraft

5. Post Stall Propeller Behavior at Low Reynolds Numbers

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1. The Aerodynamics and Hover Control for the X-wing VTOL MAV;Proceedings of 2021 International Conference on Autonomous Unmanned Systems (ICAUS 2021);2022

2. Visualization of vortical flows around a rapidly pitching wing and propeller;International Journal of Micro Air Vehicles;2017-02-02

3. Comparison of wing–propeller interaction in tractor and pusher configuration;International Journal of Micro Air Vehicles;2016-03

4. Aerodynamic Characteristics of a Low Aspect Ratio Wing and Propeller Interaction for a Tilt-Body MAV;International Journal of Micro Air Vehicles;2013-12

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