How to Calculate Weight of aircraft for given required power?
Weight of aircraft for given required power calculator uses Weight=Power*lift coefficient/(Freestream Velocity*Drag Coefficient) to calculate the Weight, The Weight of aircraft for given required power in a steady, level flight is a function of freestream velocity and aerodynamic coefficients. Weight and is denoted by W symbol.
How to calculate Weight of aircraft for given required power using this online calculator? To use this online calculator for Weight of aircraft for given required power, enter Power (P), lift coefficient (C_{L}), Freestream Velocity (V_{∞}) and Drag Coefficient (C_{D}) and hit the calculate button. Here is how the Weight of aircraft for given required power calculation can be explained with given input values -> 0.1 = 100*10/(100*100).