Aerodynamics and Flight Mechanics (5cr)
Code: 5K00CQ13-3004
General information
- Enrolment period
- 02.12.2017 - 11.01.2018
- Registration for the implementation has ended.
- Timing
- 01.01.2018 - 31.07.2018
- Implementation has ended.
- Credits
- 5 cr
- Mode of delivery
- Contact learning
- Unit
- Mechanical Engineering
- Campus
- TAMK Main Campus
- Teaching languages
- Finnish
- Degree programmes
- Degree Programme in Mechanical Engineering
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
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