Abstract
The study investigates the aerodynamic characteristics of the supercritical RAE2822 airfoil with a Gurney flap using computational fluid dynamics (CFD). The research analyzes the effects of different Gurney flap heights (1%c, 2%c, and 3%c) and mounting angles (30°, 45°, 60°, 75°, and 90°) on the lift and drag coefficients. The results indicate that increasing the Gurney flap height enhances the lift coefficient and shifts the shock waves downward, while the drag coefficient increases for positive angles of attack and decreases for negative angles of attack. The study validates the computational results with experimental data, showing good agreement.
Keywords
Aerodynamic Characteristics
Drag coefficient
Gurney flap
lift enhancement
RAE2822
Supercritical Airfoil