Stress and deflection analysis; fatigue, safe life, damage tolerant design. Propulsion systems integration; landing gear; control and other subsystems. Mechanical component design. Airworthiness regulations and certification procedures. Weight and cost estimation and control. System reliability. Design studies of aircraft or spacecraft components. Prerequisite(s): MAAE 3202 and AERO 3002.Lectures three hours a week, problem analysis three hours a week.
Stress and deflection analysis; fatigue, safe life, damage tolerant design. Propulsion systems integration; landing gear; control and other subsystems. Mechanical component design. Airworthiness regulations and certification procedures. Weight and cost estimation and control. System reliability. Design studies of aircraft or spacecraft components. Prerequisite(s): MAAE 3202 and AERO 3002.Lectures three hours a week, problem analysis three hours a week.