Course Information

Course Name	Turkish	Hesaplamalı Aerodinamik
	English	Computational Aerodynamics
Course Code	UCK 419E	Credit	Lecture (hour/week)	Recitation (hour/week)	Laboratory (hour/week)
Semester	7	3	3	-	-
Course Language		English
Course Coordinator		Fırat Oğuz Edis
Course Objectives		1. To be able to calculate incompressible 2D potential flows around airfoils by using panel methods 2. To be able to calculate incompressible 3D potential flows around finite wings by using panel methods 3. To be able to calculate incompressible 3D potential flows around aircraft bodies by using panel methods
Course Description		Fundamentals of inviscid incompressible flow, general solution of incompressible potential flow equations, Panel methods, singularity elements and influence coefficients, two dimensional numerical solutions, three dimensional numerical solutions.
Course Outcomes		Student, who passed the course satisfactorily can: 1. be understand 2- and 3-Dimensional potential flow problems, its modeling by integral equations and boundary conditions 2. be able to calculate a thin airfoil problem by using a lumped vortex method 3. be able to calculate a thick airfoil problem by using a surface singularity method 4. be able to calculate a wing problem by using vortex lattice method 5. be able to calculate an aircraft body problem by using panel method
Pre-requisite(s)		Students are expected to have basic knowledge of aerodynamics and programming.
Required Facilities		Personal Computer/Laptop
Other
Textbook		1) Joseph Katz, Allen Plotkin, Low-Speed Aerodynamics: From Wing Theory to Panel Methods, McGraw-Hill, 1991
Other References		1) Sinan Kalkan, Onur T. Şehitoğlu, Göktürk Üçoluk, Programming with Python for Engineers, Springer e-book

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