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UCK 351E
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Course Information
Course Name
Turkish
Aerodinamik
English
Aerodynamics
Course Code
UCK 351E
Credit
Lecture
(hour/week)
Recitation
(hour/week)
Laboratory
(hour/week)
Semester
5

3
1

Course Language
Turkish
Course Coordinator
Ayşe Gül Güngör
Course Objectives
1.To give the fundamentals of incompressible aerodynamics
2.To solve basic aerodynamics problems
Course Description
Aerostatic. Aerodynamic forces and moments. Fundamental principles and
equations. Flow types. Potential flow approach. One dimensional potential
flows. Airfoil aerodynamics. Two dimensional potential flows. Thin airfoil
theory, 2D panel methods. Finite wing theory. 3D incompressible flow
Course Outcomes
Student, who passed the course satisfactorily can:
Know the basic equations for inviscid incompressible flow
Apply conservation of mass and momentum equations to control volume
Find the potential and stream functions for the flow around bosies and
calculate the pressure distribution
Calculate the lift and moment coefficients by using thin airfoil theory
Calculate the lift and drag for finite wings at different planforms
Prerequisite(s)
AKM 204 MIN FF OR AKM 204E MIN FF
Required Facilities
Other
Textbook
Anderson, J.D., 2001, Fundamentals of Aerodynamics, McGrawHill,
ISBN:0072950463.
Other References
Houghton, E.L. and Carpenter, P.W., 2003, Aerodynamics for Engineering
Students, ButterworthHeinemann, ISBN:0750651113.
Bertin, J.J and Smith, M.L., 2008, Aerodynamics for Engineers, PrenticeHall,
ISBN:0132272687.
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