Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity evaluator uses Velocity at a Point = sqrt(Freestream Velocity^2*(1-Pressure Coefficient)) to evaluate the Velocity at a Point, Velocity at point on airfoil for given pressure coefficient and free-stream velocity formula is product of free stream velocity into square root of one minus pressure coefficient in incompressible flow. Velocity at a Point is denoted by V symbol.
How to evaluate Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity using this online evaluator? To use this online evaluator for Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity, enter Freestream Velocity (u∞) & Pressure Coefficient (Cp) and hit the calculate button.