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 (Pdynamic), Reference Area (S), Zero-lift drag coefficient (CD,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)).