Home▸Fluid Dynamics & Aerodynamics▸NACA Wing on a Test Rig: Panel-Method Lift, Induced Drag and Stall

NACA Wing on a Test Rig: Panel-Method Lift, Induced Drag and Stall

Interactive 3D NACA 0012, 2412 and 4412 wing on a Blender-built test rig: Hess-Smith panel method with Kutta condition, pressure coloured surface, finite-wing downwash and induced drag, Viterna post-stall model and four in-page numerical checks.

Fluid Dynamics & Aerodynamics3DModerate60 FPS📱 Mobile-adapted🟠 Blender💨 Air & Wind ⇄ 2D version

⚙ Under the hood

Interactive 3D NACA 0012, 2412 and 4412 wing on a Blender-built test rig: Hess-Smith panel method with Kutta condition, pressure-coloured surface, finite-wing downwash and induced drag, Viterna post-stall model and four in-page numerical checks.

aerodynamicsNACAliftdragangle of attackBernoullistall

3D · Three.js / WebGL renderer · 60 FPS target · runs fully client-side, no install