2. Requirements of aircraft design (2 credit hours)
3. Aircraft conceptual design: weight estimation, Payload-range diagrams (2 credit hours)
4. Aircraft conceptual design: wing loading and thrust-weight ratio (2 credit hours)
5. Analysis of configurations (2 credit hours)
6. Aircraft preliminary design: wing design and propulsion system design (2 credit hours)
7. Aircraft preliminary design: fuselage design (2 credit hours)
8. Aircraft preliminary design: undercarriage design and empennage design (2 credit hours)
Practice:
4. Analysis of tasks and market; determination of design requirements (4 credit hours)
5. Weight estimation (4 credit hours)
6. Payload-range diagrams, wing loading and thrust loading (4 credit hours)
7. Determination of aerodynamic configuration (4 credit hours)
8. Wing design (4 credit hours)
9. Integration of propulsion system (6 credit hours)
10. Fuselage design (6 credit hours)
11. Undercarriage design and empennage design (6 credit hours)
12. Analysis of flight Control and stability (6 credit hours)
13. Design of control system (6 credit hours)
14. Structure analysis (6 credit hours)
15. Analysis of cost and effectiveness (6 credit hours)
16. Oral presentation (2 credit hours)
教材 (Textbook)
[1] 李为吉,王正平,艾剑良,杨华保,飞机总体设计,西北工业大学出版社,2004。
[2] Raymer, D.P., Aircraft design: A conceptual approach, 3rd edition, AIAA Education series, American Institute of
Aeronautics and Astronautics, 1989.