How to Calculate Minimum Thrust required for given weight?
Minimum Thrust required for given weight calculator uses Thrust = (Dynamic Pressure*Area*Zero Lift Drag Coefficient)+((Weight of Body^2)/(Dynamic Pressure*Area*pi*Oswald Efficiency Factor*Aspect Ratio of a wing)) to calculate the Thrust, The Minimum Thrust required for given weight for a steady, level flight is the force that moves an aircraft through the air. Thrust is used to overcome the drag of an airplane, and to overcome the weight of a rocket. Thrust 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), Area (A), Zero Lift Drag Coefficient (CD,0), Weight of Body (Wbody), Oswald Efficiency Factor (e) & 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 -> 75.70435 = (10*20*0.31)+((221^2)/(10*20*pi*0.51*4)).