Generation of a mesh mesh = SF_Mesh( 'NacaFourDigits_Mesh.edp', 'Options', 'xlim', 'ylim',) WARNING - Detected verbosity = 4 in Publish mode not recommended ! switching to 2 instead
VISCOUS FLOW (Re = 1000 and 10 000 alpha = 0)įlow around a wing profile : example for a NACA0012 profile close all Airfoils with a series number beginning with 00 such as the NACA 0012 - are symmetrical and have no camber.Computing flow for alpha = 20 degrees with right circulation (Kutta condition verified).