Description
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
- Prerequisite(s): AERO 3002 and MATH 3705 .
Conditions and arrangements
- Prerequisite(s): AERO 3002 and MATH 3705 .
- Lectures three hours a week, problem analysis three hours a week.
Reference text in its original language
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): AERO 3002 and MATH 3705 .
- Lectures three hours a week, problem analysis three hours a week.
Sources and references
Dates and sources are retained to help you verify the information. Translations are provided to facilitate reading; the official source governs conditions and requirements.
Source reference : https://calendar.carleton.ca/undergrad/courses/AERO/