What is it about?
Small Unmanned Aerial Vehicles (UAVs) fly at low speed and near to the ground. As such, the flow over their wings can easily separate. This paper investigates how a potential criterion for flow separation varies with the rate at which the wing pitch angle is changed.
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This page is a summary of: Low-Reynolds Number Behavior of the Leading-Edge Suction Parameter at Low Pitch Rates, AIAA Journal, September 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j060733.
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