EXPERIMENTAL CHARACTERIZATION AND AEROELASTIC ANALYSIS OF A COMPOSITE WING

Abstract

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In the rapidly evolving landscape of aviation, Unmanned Aerial Vehicles (UAVs) have established a niche for themselves, finding applications in diverse sectors such as military operations, aerial photography, surveying, agriculture, and even delivery services. Central to the functionality of a UAV is its wing, a component that plays a pivotal role in ensuring the UAV's flight stability, control, and efficiency

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