Abstract
The default values for the maximum pitch and yaw speeds from CS 23.371, seem to be too conservative that would result in overstressing of the structure.A simplified dynamic simulation is proposed to evaluate more confident velocities for a specific aircraft. The yawing condition is related to the sudden rudder deflection and a maneuver with lateral gust. The pitching conditions are a result of a sudden elevator deflection. The model takes into account the nonlinear effects of the aerodynamic coefficients and controls efficiencies.
Full Text
Published Version
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call