Simulation Modelling for Computer Aided Design of Secondary Aerodynamic Wing Surfaces

Abstract

The simulation modelling technique of secondary aerodynamic wing surface of the long-haul aircraft using a high-precision mathematical simulation in the aerodynamics and hydrodynamics computer programme has been formulated in the present article. The method proposed is based on the modern methods in the field of computer-aided design of aircraft using CATIA three-dimensional simulation and simulation modelling in SALOME environment. The use of high-precision mathematical simulation in computer-aided design of secondary aerodynamic wing surfaces allows us to determine the aerodynamic characteristics of the secondary aerodynamic surface of the model developed and to verify the previous results of the project definition.