How to Calculate Lift of Wing given Circulation at Origin?
Lift of Wing given Circulation at Origin calculator uses Lift Force = (pi*Freestream Density*Freestream Velocity*Wingspan*Circulation at Origin)/4 to calculate the Lift Force, The Lift of Wing given Circulation at Origin formula calculates the lift for the elliptical lift distribution along the wingspan when the circulation at the origin is given. Lift Force is denoted by FL symbol.
How to calculate Lift of Wing given Circulation at Origin using this online calculator? To use this online calculator for Lift of Wing given Circulation at Origin, enter Freestream Density (ρ∞), Freestream Velocity (V∞), Wingspan (b) & Circulation at Origin (Γo) and hit the calculate button. Here is how the Lift of Wing given Circulation at Origin calculation can be explained with given input values -> 488.5416 = (pi*1.225*15.5*2.34*14)/4.