AERO 4003
Aerospace Systems Design
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.
Prerequisites & course information
Prerequisite(s): AERO 3002 and MATH 3705 . Lectures three hours a week, problem analysis three hours a week.
Sources
- Course catalogue ↗2026–2027