Convergence of lift force calculation of a tapered wing using non-linear section data

Abstract

The article presents some peculiarities of lift force calculation method using nonlinear section data. The main task is to determine an influence of iteration procedure on solution accuracy. This evaluation is a part of initiated research on potentials and application limits of the method. Set of accuracy is described in more details. Influence results of iteration procedure are presented for lift calculation of a tapered wing.