Enter your Velocity, Wing Reference Area, Coefficient of Lift (Cl), and Air Density (or set a Custom Air Density) into the Downforce Calculator to find the Downforce and Dynamic Pressure pushing your vehicle into the road.
Downforce
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Downforce
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Dynamic Pressure
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Wing downforce is calculated using the formula: Downforce = ½ × ρ × A × Cl × V². This accounts for air density (ρ), wing area (A), lift coefficient (Cl), and velocity squared (V²).
For downforce applications, the coefficient of lift is typically negative or inverted. Racing wings commonly have Cl values between -1.0 to -3.0, with higher absolute values producing more downforce.
Downforce directly translates to additional tire grip. Every pound of downforce adds approximately one pound of effective weight pressing the tires to the road, increasing available traction for cornering and braking.
Aerodynamic forces increase exponentially with speed due to the V² relationship. Doubling your speed results in four times the downforce, which is why high-speed aerodynamics are so critical in motorsports.
Use sea level air density (0.00238 slug/ft³) for standard conditions. Air density decreases with altitude and increases with lower temperatures, affecting downforce output by the same proportion.
Wing reference area is typically the planform area (top-down view) of the wing surface. For multi-element wings, include the total projected area of all elements including flaps and endplates.
Downforce is simply negative lift. While aircraft wings generate upward lift, racing wings are designed inverted to push the vehicle down, improving traction and handling at high speeds.
Theoretical calculations provide good estimates, but real-world results vary due to ground effects, wing interactions, and air quality. Wind tunnel testing or CFD analysis gives more precise values for specific applications.