How to Calculate Moment Coefficient about Leading-Edge for Symmetrical Airfoil by Thin Airfoil Theory?
Moment Coefficient about Leading-Edge for Symmetrical Airfoil by Thin Airfoil Theory calculator uses Moment Coefficient about Leading Edge = -Lift Coefficient/4 to calculate the Moment Coefficient about Leading Edge, The Moment coefficient about leading-edge for symmetrical airfoil by Thin airfoil theory formula is obtained as the one-fourth of the lift coefficient. Moment Coefficient about Leading Edge is denoted by Cm,le symbol.
How to calculate Moment Coefficient about Leading-Edge for Symmetrical Airfoil by Thin Airfoil Theory using this online calculator? To use this online calculator for Moment Coefficient about Leading-Edge for Symmetrical Airfoil by Thin Airfoil Theory, enter Lift Coefficient (CL) and hit the calculate button. Here is how the Moment Coefficient about Leading-Edge for Symmetrical Airfoil by Thin Airfoil Theory calculation can be explained with given input values -> -0.3 = -1.2/4.