Course Information

Course Name	Turkish	Aerodinamik
	English	Aerodynamics
Course Code	UCK 351	Credit	Lecture (hour/week)	Recitation (hour/week)	Laboratory (hour/week)
Semester	-	-	3	1	-
Course Language		Turkish
Course Coordinator		Mahmut Adil Yükselen
Course Objectives		1. To give the fundamental concepts of aerodynamics 2. Solve fundamental aerodynamics problems
Course Description		Aero-statics, Aerodynamic forces and moments. Fundamental principles and equations. Potential flow approximation. Flow types. One dimensional non-viscous flows. Airfoil aerodynamics. Two dimensional potential flows. Thin airfoil theory. Two-dimensional panel methods. Finite wing theory. Three-dimensional 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 Fluid Mechanics min DD
Required Facilities
Other
Textbook		Anderson, J.D., 2001, Fundamentals of Aerodynamics, McGraw-Hill,
Other References