Aerodynamics and flight mechanics (5 cr)
Code: 5K00CQ13-3001
General information
- Enrolment period
- 01.12.2015 - 15.05.2016
- Registration for the implementation has ended.
- Timing
- 01.01.2016 - 30.06.2016
- Implementation has ended.
- Credits
- 5 cr
- Mode of delivery
- Contact learning
- Unit
- Mechanical Engineering
- Campus
- TAMK Main Campus
- Teaching languages
- Finnish
Objectives (course unit)
TTY is responsible of the content and objectives of the course.
The student knows and understands:
• Flow phenomena and different types of flows in aircraft engineering
• 2- and 3-dimension analysis of wing
• Aerodynamics of fuselage and aircraft as a whole
• Stability and control
• Symmetrical and asymmetrical movement
• Dynamical stability and special situations
• Aeroelastic phenomena
• Base for performance analysis
• Instaneous and long-term performance values
• Basics of flight simulation and control systems
• Aerodynamics and flight mechanics of helicopters
Content (course unit)
TTY is responsible of the content and objectives of the course.
• Flow phenomena and different types of flows in aircraft engineering
• 2- and 3-dimension analysis of wing
• Aerodynamics of fuselage and aircraft as a whole
• Stability and control
• Symmetrical and asymmetrical movement
• Dynamical stability and special situations
• Aeroelastic phenomena
• Base for performance analysis
• Instaneous and long-term performance values
• Basics of flight simulation and control systems
• Aerodynamics and flight mechanics of helicopters
Assessment scale
0-5
Further information
TTY is responsible of the content and objectives of the course.
Litterature:
Houghton E.L., Carpenter P.W., Aerodynamics for Engineering Students, 5th Edition, 2003