Maximum stationary flight duration =
Please note : this modelisation is a first approach for information purpose. IMPORTANT : the autonomy is proportional to the propellers diameters.
formula : (mass flow): dm = 1/2 * rho * Surface * V (power flow): Power = 1/2 * dm * V² Traction = dm * V ... (absorbed power) Pa = 1/4 * rho * Surface * (2 * Traction / (rho * Surface))^(3/2)