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✈️ Airfoil Wind Tunnel Simulator

Configure airfoil + wind tunnel → visualize airflow, lift & drag

🔧 Airfoil Settings

Chord Length (m)

Thickness (% of chord)

Camber (% of chord)

Angle of Attack (°)

Wing Span (m)

Wind Speed (km/h)

Air Temperature (°C)

Altitude (m)

Streamline Density 25 lines

Particle Trail Length 80

Air Density:—

Dynamic Pressure:—

Reynolds Number:—

Mach Number:—

Lift:—

Drag:—

Lift/Drag Ratio:—

Cl (Lift Coeff):—

Cd (Drag Coeff):—

Status:Idle

Based on thin airfoil theory + potential flow. Air flows faster over the curved top surface → lower pressure (Bernoulli) → lift.

High angle of attack causes stall — flow separation and dramatic lift loss.