Dynamika samolotu po symetrycznym zrzucie podwieszeń z zastosowaniem symulacji numerycznej

The dynamics of longitndinal motion of a jet aeroplane perturbed by a drop of suspended loads has been studied. The complete set of nonlinear equations of motion has been applied. Programs have been prepared for numerical integration of equations of motion by the Runge-Kutta method. A series of calculations have been performed. Calculation results demonstrate the character of perturbations of the aeroplane motion after a drop of loads.