Optimized Design and Analysis of an Amphibious Flying Wing UAV - S, Prasanth;K, Yokesvaran;A, Surenderpaul
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This study focuses on the optimized design and analysis of an amphibious flying wing Unmanned Aerial Vehicle (UAV). The innovative design integrates aerodynamic efficiency, stability, and operational versatility for both aerial and aquatic environments. Computational tools were utilized to refine the air frame and hydrodynamic features, ensuring seamless transitions between land, air, and water operations. Key performance parameters, including lift-to-drag ratio, structural integrity, and buoyancy, were evaluated to enhance functionality. The optimized design aims to support diverse…mehr

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Produktbeschreibung
This study focuses on the optimized design and analysis of an amphibious flying wing Unmanned Aerial Vehicle (UAV). The innovative design integrates aerodynamic efficiency, stability, and operational versatility for both aerial and aquatic environments. Computational tools were utilized to refine the air frame and hydrodynamic features, ensuring seamless transitions between land, air, and water operations. Key performance parameters, including lift-to-drag ratio, structural integrity, and buoyancy, were evaluated to enhance functionality. The optimized design aims to support diverse applications such as surveillance, search and rescue, and environmental monitoring, showcasing the potential for multi functional UAV systems in challenging terrains.
Autorenporträt
 Mr. S. Prasanth serves as an Assistant Professor in Aerospace Engineering at Agni College of Technology, Chennai, Tamil Nadu, India. With a decade of teaching experience, he holds an M.E. in Aerospace Technology from the MIT, Anna University, Chennai, Tamilnadu, India.His areas of interest include Propulsion and Aerodynamics and High Speed Jets.