How to Calculate Minimum Thrust required for given lift coefficient?
Minimum Thrust required for given lift coefficient calculator uses Thrust of an aircraft=Dynamic Pressure*Area*(Zero-lift drag coefficient+((lift coefficient^2)/(pi*Oswald efficiency factor*Aspect Ratio of a wing))) to calculate the Thrust of an aircraft, The Minimum Thrust required for given lift coefficient in a steady, level flight is a function of the lift coefficient and the zero-lift drag coefficient of aircraft. Thrust of an aircraft and is denoted by T symbol.
How to calculate Minimum Thrust required for given lift coefficient using this online calculator? To use this online calculator for Minimum Thrust required for given lift coefficient, enter Dynamic Pressure (P_{dynamic)}, Area (A), Zero-lift drag coefficient (C_{D,0}), lift coefficient (C_{L}), Oswald efficiency factor (e) and Aspect Ratio of a wing (AR) and hit the calculate button. Here is how the Minimum Thrust required for given lift coefficient calculation can be explained with given input values -> 7965.797 = 10*50*(0.0161+((10^2)/(pi*0.5*4))).