Flight Dynamics and Basics of Aircraft Assembly. Handbook for Aeronautical Students

      Аннотация: The mechanics of the flight studies the forces acting on the aircraft in flight, and the reaction of the aircraft to the action of these forces. All aircrafts are equipped with a control system that allows the pilot to maneuver and release forces from the control levers on each of the three axes. The aerodynamic moments required to rotate the aircraft are usually realized by deflecting control surfaces that change the curvature of the profile. Control surfaces are located as far as possible from the center of gravity in order to create the maximum control moment.

Ключевые слова: flight dynamics, Calculation aerodynamic characteristics of the aircraft AN-225, Thrust Required and Thrust Available, practical ceiling of aircraft, building a polar flight, Coefficient of aerodynamic lift, the angle of inclination of the trajectory, aerodynamic drag coefficient of planning, the angel of decline associated with the aerodynamic efficiency, the angle of trajectory planning, building Berth, Structural and technological characteristics of the assembly unit.