UCK 419E - Computational Aerodynamics

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.