Course Information

Course Name	Turkish	Aerodinamik
	English	Aerodynamics
Course Code	UCK 305E	Credit	Lecture (hour/week)	Recitation (hour/week)	Laboratory (hour/week)
Semester	-	3	3	-	-
Course Language		English
Course Coordinator		Melike Nikbay Melike Nikbay
Course Objectives		1. To give the fundamentals of incompressible aerodynamics 2. To solve basic aerodynamics problems
Course Description		Aerodynamic forces and moments, fundamental principles and equations, flow types, potential flow approach, airfoils, finite wings.
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 bodies and calculate the pressure distribution, 4. calculate the lift and moment coefficients by using thin airfoil theory, 5. calculate the lift and induced drag of finite wings, apply for wings of different planforms,
Pre-requisite(s)		AKM 204/E or AKM 205/E or AKM 214/E or AKM 215/E or AKM 219/E, MIN DD
Required Facilities
Other
Textbook		Fundamentals of Aerodynamics, John D. Anderson, Jr. Christopher P. Cadou
Other References		Aerodynamics for Engineering Students, E.L. Houghton, P.W. Carpenter, Steven H. Collicott, Daniel T. Valentine, Aerodynamics for Engineers, John J. Bertin • Russell M. Cummings