This project involves the design, fabrication, and testing of a remote-controlled canard wing aircraft model. The primary aim is to demonstrate the operation of the aircraft and determine pressure and attitude differences during flight using wind tunnel testing.
- Design: Utilized CATIA V5 for designing the canard wing with NACA 2412 airfoil.
- Fabrication: Employed 3D printing techniques and materials such as ABS and Styrofoam.
- Testing: Conducted wind tunnel tests to analyze pressure distribution and flow characteristics.
- Results: Achieved higher angles of attack with improved maneuvering capabilities and minimized flow separation.
- CATIA V5
- XFLR5 for airfoil performance comparison
- 3D Printing (FDM method)
- Arduino for sensor integration
- Wind tunnel for testing