How to Calculate Lift Coefficient for given wing loading and turn radius?
Lift Coefficient for given wing loading and turn radius calculator uses Lift Coefficient = 2*Wing Loading/(Freestream density*Turn Radius*[g]) to calculate the Lift Coefficient, The Lift Coefficient for given wing loading and turn radius depends upon the altitude, turn radius, and wing loading of the aircraft. Lift Coefficient is denoted by CL symbol.
How to calculate Lift Coefficient for given wing loading and turn radius using this online calculator? To use this online calculator for Lift Coefficient for given wing loading and turn radius, enter Wing Loading (WS), Freestream density (ฯโ) & Turn Radius (R) and hit the calculate button. Here is how the Lift Coefficient for given wing loading and turn radius calculation can be explained with given input values -> 0.002775 = 2*5/(1.225*300*[g]).