Concentrated on unmanned vehicle development, especially CAD design, and I’m eager to contribute to R&D of UAV airframes and propulsion.
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This project focuses on the design, aerodynamic analysis, and performance evaluation of a fixed-wing UAV manufactured using PLA material. The study includes airfoil selection, wing configuration design, CFD simulations, stability analysis, and performance estimation. XFLR5 and ANSYS Fluent were utilized to evaluate lift, drag, pressure distribution, and flight characteristics under various operating conditions. The objective is to develop an efficient and manufacturable UAV platform suitable for research and educational purposes.
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