Aerodynamic study on bio-inspired unmanned aerial vehicle wings

被引:0
|
作者
Rajamurugu, N. [1 ]
机构
[1] KCG Coll Technol, Dept Aeronaut & Aerosp Engn, Chennai, Tamilnadu, India
关键词
bio-inspired wing; experimental aerodynamics; analysis of variance; ANOVA; optimisation; wind tunnel;
D O I
10.1504/IJSA.2024.142567
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This study investigates the aerodynamic performance of bio-inspired wings for unmanned aerial vehicles (UAVs). Five insect-inspired wings - Tipula SP, dragonfly, hawkmoth, honey bee, and American deer botfly - were tested across varying angles of attack (0 degrees, 5 degrees, 10 degrees, 15 degrees), wind velocities (5 m/s, 10 m/s, 15 m/s), and flapping frequencies (2 Hz, 4 Hz) in a wind tunnel. The findings reveal that the Tipula SP wing design is the most effective, achieving a maximum lift coefficient (Cl) of 1.689 at 15 m/s, a 15 degrees angle of attack, and a 4 Hz frequency. This performance is 18.01% higher than dragonfly wings, 69.78% higher than hawkmoth wings, 95.20% more efficient than honey bee wings, and 78.21% greater than American deer botfly wings under the same conditions. The significant lift generation by Tipula SP underscores its potential to enhance agility and manoeuvrability in MAVs, especially within confined spaces.
引用
收藏
页数:23
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