Sensitivity analysis of airfoil aerodynamics during pitching motion at a Reynolds number of 1.35x10(5) KU Leuven
© 2018 The Authors Numerically reproducing wind tunnel experimental tests of flow behavior around a pitching airfoil is a challenge, especially under the occurrence of dynamic stall at relatively high angles of attack. This not only requires the application of advanced turbulence models, but also asks for examining the influence of the most relevant model parameters in detail. This contribution presents the results of an extensive computational ...