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, Lift Coefficient for given wing loading and turn radius formula is defined as a measure of the aerodynamic efficiency of an aircraft during high load factor maneuvers, relating wing loading, turn radius, and the surrounding air density. 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 (ρ∞) & 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 -> 0.002015 = 2*354/(1.225*29495.25*[g]).