How to Calculate Lift Coefficient for a given wing loading and turn radius?
Lift Coefficient for a 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 a given wing loading and turn radius depends upon the altitude, turn radius and wing loading of the aircraft. lift coefficient and is denoted by C_{L} symbol.
How to calculate Lift Coefficient for a given wing loading and turn radius using this online calculator? To use this online calculator for Lift Coefficient for a given wing loading and turn radius, enter Wing Loading (W_{S}), Freestream density (ρ_{∞}) and Turn Radius (R) and hit the calculate button. Here is how the Lift Coefficient for a given wing loading and turn radius calculation can be explained with given input values -> 0.002775 = 2*5/(1.225*300*[g]).