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Published on: April 23, 2018
Covert-inspired flaps for lift enhancement and stall mitigation.
1University of Illinois at Urbana-Champaign, 105 S. Mathews Ave., Urbana, IL 61801, United States of America.
A bird-inspired covert flap can delay stall by 5° and increase post-stall lift by 23% for unmanned aerial vehicles (UAVs). This flow control device shows tunable effectiveness on sharp stall airfoils but acts as a simple on/off switch for soft stall airfoils.
Area of Science:
- Aerospace Engineering
- Fluid Dynamics
- Bio-inspired Design
Background:
- Unmanned aerial vehicles (UAVs) exhibit limitations in adaptability and agility compared to birds, especially at low Reynolds numbers.
- Bird's covert feathers act as natural flow-control devices, mitigating flow separation, enhancing lift, and delaying stall.
- Understanding these biological mechanisms can inform the design of more effective UAVs.
Purpose of the Study:
- To investigate the effects of a covert-inspired flap on airfoil performance at Reynolds numbers relevant to small UAVs (10^5).
- To analyze how flap chord-wise location and deflection angle influence lift and drag on airfoils with distinct stall characteristics (sharp vs. soft).
- To compare the performance of freely-moving and static covert-inspired flaps.
Main Methods:
- Wind tunnel experiments were conducted on two airfoils: NACA 2414 (sharp stall) and E387(A) (soft stall).
- Numerical simulations were employed to analyze the aerodynamic principles behind the flap's effects.
- Investigated static and freely-moving flaps with varying chord-wise positions and deflection angles.
Main Results:
- The static covert-inspired flap successfully delayed stall by up to 5° and improved post-stall lift by up to 23%.
- Stall delay and lift enhancement were highly dependent on the airfoil's stall characteristics.
- For sharp stall airfoils, lift improvements were tunable via flap deflection and effective across various locations; for soft stall airfoils, the flap's effectiveness was limited and insensitive to adjustments.
Conclusions:
- The covert-inspired flap demonstrates significant potential as a flow control device for UAVs.
- Its effectiveness is tunable for sharp stall airfoils, offering versatile aerodynamic control.
- For soft stall airfoils, the flap serves primarily as a stall mitigation device with a binary on/off functionality.
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