École Nationale Supérieure de
Techniques Avancées

Abstract

In this report is presented our prospection in the relatively novel field of study that is the propulsion by electroaerodynamical flow created by a corona discharge, confined between two flat wings. In order to compute the friction around the wings, we first introduce the boundary layer theory and try to develop a code that solves the boundary layer with the integral method. We try to apply it in the case of a flow of electroaerodynamic wind. Finally we create models of the wall shear stress along the flat plates.