use of a modern airfoil code (XFOIL) for analysis of airfoils and a second programming assignment project for studying the effect of superposing different elementary flow solutions using a numerical approach with visualization using modern software (Matlab). Contribution of course to meeting the requirements of Criterion 5 - math and basic X. Mauclère, Automatic 2D airfoil generation, evaluation and optimisation using MATLAB and XFOIL [M.S. thesis], Department of Mechanical Engineering, Section of Fluid Mechanics, Technical University of Denmark, Lyngby, Denmark, 2009.
XFOIL results. Thesis is also concerned with brief description of XFOIL and MATLAB, description of profile characteristics and comparison numbers used in calculation by XFOIL. Klíčová slova XFOIL, MATLAB, integrace, profil, polára, vztlaková čára XFOIL, MATLAB, integration, profile, polar curve, lift curve Vysoké učení technické v Brně