Aerodynamic Modelling and Fabrication of Multi Task Delta Wing UAV
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Abstract
This article emphasises the design, analysis and fabrication of a fighter jet combat UAV featuring a delta wing configuration, renowned for its high manoeuvrability and maximum performance in aerial combat scenarios. The process begins with the design phase, where the UAV is modelled using CAD software. The fabrication involves moulding techniques, utilising foam as the primary material, reinforced with a fiberglass sandwich panel for enhanced strength. Subsequently, static structural analysis and wing aerodynamic simulations at a constant velocity of 15 m/s are conducted using ANSYS FLUENT. This comprehensive approach integrates cutting-edge design tools, innovative fabrication techniques and advanced computational analysis to advance fighter jet combat UAV development.
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