Desenvolvimento de ferramenta para o pós-processamento de carregamentos aerodinâmicos de asa de Veículo Aéreo Não Tripulado

Abstract

This study aims to perform an aerodynamic analysis on a AeroDesign wing using the Vortex Lattice Method [VLM] and develop a tool for the post processing of aerodynamic loads, since the methods used so far by the UFJF competition team are very time consuming, which delays the project development. Using the position at the cartesian plan, normal vector components, area and pressure coefficient of each panel from the analysis, were calculated using an algorithm the lift, bending and torsor moment along the span. The goal was achieved with great satisfaction, reducing the time consumed by about 85% and calculating the pressure force in comand surfaces, aerodynamic load which was not calculable throght the traditional method.