Modelagem numérica por elementos finitos para simulação estrutural da asa de uma aeronave leve

Abstract

This work emerged as an internship activity with a private company. The purpose is to do structural analysis on an RV-10 wing in order to confirm that its components can support the loads generated in flight. For this, the wing and every single internal component were built in detail in CAD and CAE plataforms. The strategy used to reach the goals was to submit the finite element model to three differente analysis, as: one modal analysis and two static analysis. So, results were extracted to show the stress distribution along each component and, thus, conclude about the margin in relation to the mechanical properties of the material from which it’s made.