How to Calculate Minimum Thrust required?
Minimum Thrust required calculator uses Thrust of an aircraft=Dynamic Pressure*Area*(Zero-lift drag coefficient+Coefficient of drag due to lift) to calculate the Thrust of an aircraft, The Minimum Thrust required for a steady, level flight is equal to the sum of drag due to zero lift and drag due to lift. Thrust of an aircraft and is denoted by T symbol.
How to calculate Minimum Thrust required using this online calculator? To use this online calculator for Minimum Thrust required, enter Dynamic Pressure (P_{dynamic)}, Area (A), Zero-lift drag coefficient (C_{D,0}) and Coefficient of drag due to lift (C_{D,i}) and hit the calculate button. Here is how the Minimum Thrust required calculation can be explained with given input values -> 408.05 = 10*50*(0.0161+0.8).