Literature study and design of self- propelling wing

Abstract: This project aims to design a self-propelling ionic thrust wing, combining aerodynamics and ionic propulsion technology. The system utilizes ionized particles for propulsion, generating thrust by interacting with a charged grid. The wings design incorporates lightweight materials and aerodynamic principles to optimize lift and efficiency. The integration of advanced control systems ensures stable flight, while the ionic thrusters provide a clean and efficient means of propulsion. This innovative approach holds potential for unmanned aerial vehicles with extended flight endurance and reduced environmental impact. The system utilizes a compact and efficient propulsion mechanism to generate thrust. The design also focuses on optimizing weight distribution, control systems and propulsion efficiency to achieve stable and agile flight.

Keywords: Self-Propelling, Wing, Propulsion, Aerodynamic, Efficiency, Unmanned Aerial Vehicle, Endurance, Environmental Impact.