How to Calculate Circulation at Origin in Elliptical Lift Distribution?
Circulation at Origin in Elliptical Lift Distribution calculator uses Circulation at Origin = 2*Freestream Velocity*Reference Area Origin*Lift Coefficient Origin/(pi*Wingspan) to calculate the Circulation at Origin, The Circulation at Origin in Elliptical Lift Distribution formula calculates the circulation which is constant for the elliptical lift distribution when the coefficient of lift and the wingspan are given. Circulation at Origin is denoted by Γo symbol.
How to calculate Circulation at Origin in Elliptical Lift Distribution using this online calculator? To use this online calculator for Circulation at Origin in Elliptical Lift Distribution, enter Freestream Velocity (V∞), Reference Area Origin (S0), Lift Coefficient Origin (Cl) & Wingspan (b) and hit the calculate button. Here is how the Circulation at Origin in Elliptical Lift Distribution calculation can be explained with given input values -> 13.97911 = 2*15.5*2.21*1.5/(pi*2.34).