Abstract
This study explores the optimization of the canard aerodynamic scheme by integrating wing-mounted propulsion systems to enhance efficiency. Key objectives include stability, controllability, and reducing frontal air resistance by employing an advanced aerodynamic scheme that effectively utilizes the wake filling phenomenon behind the wing when integrated with wing-mounted propulsion. The study emphasizes strategic design considerations for the wing, fuselage, and adjacent aerodynamic surfaces, which can enhance aerodynamic characteristics. Preserving the Coanda effect creates a low-pressure zone, improving overall efficiency. The paper underscores the importance of lightweight construction for safety and reliability. Numerical modeling underscores the need for physical experiments to validate results. Experimental simulations indicate possibilities for stable and controlled flight. Lightweight, reliable designs, and cutting-edge aerodynamic concepts offer prospects for improved efficiency and flight productivity.
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