How to Calculate Minimum Thrust required for given weight?
Minimum Thrust required for given weight calculator uses Thrust of an aircraft=(Dynamic Pressure*Reference Area*Zero-lift drag coefficient)+((Weight^2)/(Dynamic Pressure*Reference Area*pi*Oswald efficiency factor*Aspect Ratio of a wing)) to calculate the Thrust of an aircraft, The Minimum Thrust required for given weight for a steady, level flight is a function of zero-lift drag coefficient, dynamic pressure, reference area, Oswald efficiency factor, and aspect ratio of the wing of an aircraft. Thrust of an aircraft and is denoted by T symbol.
How to calculate Minimum Thrust required for given weight using this online calculator? To use this online calculator for Minimum Thrust required for given weight, enter Dynamic Pressure (P_{dynamic)}, Reference Area (S), Zero-lift drag coefficient (C_{D,0}), Weight (W), 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 weight calculation can be explained with given input values -> 32.63599 = (10*5*0.0161)+((100^2)/(10*5*pi*0.5*4)).