Course Information

Course Name	Turkish	Aerodinamik
	English	Aerodynamics
Course Code	UCK 351	Credit	Lecture (hour/week)	Recitation (hour/week)	Laboratory (hour/week)
Semester	5	-	3	1	-
Course Language		Turkish
Course Coordinator		Mehmet Fevzi Ünal
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, 2-D panel methods. Finite wing theory. 3-D incompressible flow
Course Outcomes		Student, who passed the course satisfactorily can: 1. Know the basic equations for inviscid incompressible flow 2. Apply conservation of mass and momentum equations to control volume 3. Find the potential and stream functions for the flow around bosies and calculate the pressure distribution 4. Calculate the lift and moment coefficients by using thin airfoil theory 5. Calculate the lift and drag for finite wings at different planforms
Pre-requisite(s)		AKM 204 MIN DD OR AKM 204E MIN DD
Required Facilities
Other
Textbook		Fundamentals of Aerodynamics, 3rd Ed., John D. Anderson, Jr., McGraw-Hill, 2001.
Other References		Aerodynamics for Engineering Students, 5th Ed., E.L. Houghton and P.W. Carpenter, Butterworth-Heinemann, 2003.