Estudio de algunos perfiles aerodinámicos

Abstract

If you have an wing profile through the air, this produces changes in the air velocity along the surface, this work consists of carrying out a study of the classic wing profile or also called aerodynamic profile, which corresponds to taking a wing and make a cut with a plane perpendicular to it, then said cut reveals a certain geometry, this cut is the so-called wing profile, such profiles have one end with a rounded shape and another with a sharp shape, called leading edge and trailing edge respectively , they also have a line that joins the leading edge with the trailing edge at the top, it is called upper camber and at the bottom lower camber. The development of this work is based on making some variation in the shape of the profile, either in the concavity of the leading edge, of the lower camber or the modification of the convex part of the upper camber and with these alterations being able to evaluate how the flow behaves through this new profile compared to the classic.