Welcome to the Veaero Calculator! This tool helps you calculate the lift or drag force experienced by an aircraft or airfoil based on various parameters. Input your data below to begin.
Parameters
Speed (V): The velocity of the aircraft or airfoil relative to the air.
Surface Area (S): The reference area used in calculating the force, typically the wing area for lift calculations.
Coefficient (C): The lift coefficient (Cl) or drag coefficient (Cd), which depends on the shape of the airfoil and angle of attack.
