The total aerodynamic and propulsion forces applied on an aircraft in Newtons with inertial frame K_hat positive upwards
Posted: Thu May 05, 2022 5:43 pm
The total aerodynamic and propulsion forces applied on an aircraft in Newtons with inertial frame K_hat positive upwards is given by F = 39i+ 20j+ 170k. If the mass of the aircraft is 12kg what is the acceleration of the vehicle in m/s^2.