%0 Journal Article
%T A numerical solution for the equation of the lifting surface in subsonic flow including tunnel effects
%A Adrian CARABINEANU
%A Raluca DUMITRACHE
%J INCAS Bulletin
%D 2011
%I National Institute for Aerospace Research ˇ°Elie Carafoliˇ± - INCAS
%R 10.13111/2066-8201.2011.3.3.4
%X We employ the images method to establish the lifting surface equation including tunnel effects. We obtain a 2d hypersingular integral and we utilize Gauss-type quadrature formulas to discretize it. Numerical calculations are performed for the elliptical and rectangular wings in order to calculate the jump of the pressure.
%K lifting surface
%K images method
%K hypersingular integral equation
%K tunnel effects
%K discretization
%K aerodynamic coefficients
%U http://bulletin.incas.ro/files/carabineanu_adrian_v3_is3_full.pdf