Wind Tunnel Balance Measurements of Bioinspired Tails for a Fixed Wing MAV

• Published in: Drones (Basel) Vol. 8; no. 1; p. 16
• Main Authors: Bardera, Rafael, Rodríguez-Sevillano, Ángel. A., Barroso, Estela, Matías, Juan Carlos, Sor Mendi, Suthyvann
• Format: Journal Article
• Language: English
• Published: Basel MDPI AG 01.01.2024
• Subjects: Aerodynamic coefficients; Aerodynamic drag; Aerodynamic stability; Aerodynamics; Angle of attack; balance measurements; bioinspired; bird tails; Birds; Design; Drag coefficients; Drag reduction; Efficiency; Flight; Force measurement; Longitudinal stability; Manufacturing; MAV; Measurement; Micro air vehicles (MAV); R&D; Research & development; Stabilizers (fluid dynamics); Vehicles; Weight indicators; Wind tunnel apparatus; Wind tunnels
• ISSN: 2504-446X; 2504-446X
• DOI: 10.3390/drones8010016

Bird tails play a significant role in aerodynamics and stability during flight. This paper investigates the use of bioinspired horizontal stabilizers for Micro Air Vehicles (MAVs) with Zimmerman wing-body geometry. Five configurations of bioinspired horizontal stabilizers are presented. Then, 3-component external balance force measurements of each horizontal stabilizer are performed in the wind tunnel. The Squared-Fan-Shaped Horizontal Stabilizer (HSF-tail) is selected as the optimal horizontal stabilizer that provides the highest aerodynamic efficiency during cruise flight while maintaining high longitudinal stability on the vehicle. The integration of the HSF-tail increases the aerodynamic efficiency by more than 6% up to a maximum of 17% compared to the other alternatives while maintaining the lowest aerodynamic drag value during the cruise phase. Furthermore, balance measurements to analyze the influence of the HSF-tail deflection on the aerodynamic coefficients are conducted, resulting in increased lift force and reduced aerodynamic drag with negative tail deflections. Lastly, the experimental data is validated with CFD-RANS steady simulations for low angles of attack, obtaining a relative difference on the measurement around 5% for the aerodynamic drag coefficient and around 10% for the lift coefficient during the cruise flight that demonstrates a high degree of accuracy in the aerodynamic coefficients obtained by external balance in the wind tunnel. This work represents a novel approach through the implementation of a horizontal stabilizer inspired by the structure of the tails of birds that is expected to yield significant advancements in both stability and aerodynamic efficiency, with the potential to revolutionize MAV technology.