NASA CFD Aerodynamics & Airfoil Flowfield Simulator

2D Potential Flow & Stream Function Fluid Mechanics Mechanics

Presets:
Live Flowfield Physics
Reynolds ~ 2.1e6
Lift Coefficient (CL)
0.00
Drag Coefficient (CD)
0.000
Total Lift Vector
0 N/m
Circulation (Γ)
0 m²/s

Flight Controls & Geometry

12.0°
65 m/s
15.0°
1.225 kg/m³
Display Overlays

Dynamic Aerodynamic Polar Curve CL vs CD

Export CFD Dataset
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