How to Calculate Coefficient of Lift for given thrust-to-weight ratio?
Coefficient of Lift for given thrust-to-weight ratio calculator uses lift coefficient=Drag Coefficient/Thrust-to-weight ratio to calculate the lift coefficient, The Coefficient of Lift for given thrust-to-weight ratio is given by the coefficient of drag divided by the thrust-to-weight ratio of the aircraft. lift coefficient and is denoted by CL symbol.
How to calculate Coefficient of Lift for given thrust-to-weight ratio using this online calculator? To use this online calculator for Coefficient of Lift for given thrust-to-weight ratio, enter Drag Coefficient (CD) and Thrust-to-weight ratio (T/W) and hit the calculate button. Here is how the Coefficient of Lift for given thrust-to-weight ratio calculation can be explained with given input values -> 1.666667 = 100/60.