Course Information

Course Name	Turkish	Hesaplamalı Aerodinamik
	English	Computational Aerodynamics
Course Code	UCK 419	Credit	Lecture (hour/week)	Recitation (hour/week)	Laboratory (hour/week)
Semester	-	3	3	-	-
Course Language		Turkish
Course Coordinator		Mahmut Adil Yükselen
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, unsteady incompressible potential flow, enhancement of the potential flow model.
Course Outcomes		On completing this course students should : I.be understand 2- and 3-Dimensional potential flow problems, its modeling by integral equations and boundary conditions II.be able to calculate a thin airfoil problem by using a lumped vortex method III.be able to calculate a thick airfoil problem by using a surface singularity method IV.be able to calculate a wing problem by using vortex lattice method V.be able to calculate an aircraft body problem by using panel method VI.be understand how an unsteady airfoil problem to be solved by surface singularity methods
Pre-requisite(s)		MAT 202E MIN DD and UCK 351 MIN DD
Required Facilities		to be able to use effectively at least one programming language (Fortran, MatLab, C, vBasic etc.)
Other
Textbook		J. Katz, A. Plotkin, Low-Speed Aerodynamics, From wing theory to panel methods, McGraw-Hill, Inc., 1991
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