Aeronautical Eng.design

Course content

Preliminary and detail design of aircraft. Demonstration of the design by manufacturing a reduced scale fyling model of the aircraft. Use of computer aided design tool for sizing, trade off and configuration layout studies. Landing gear design, integration of propulsion system, and structural design. Calculation of moments of inertia, weights and balance, center of gravity of the design. Static and dynamic stability, control characteristics and performance prediction of the aircraft.