Mathematical Modeling of the Design Process of Additional Aerodynamic Surfaces of the Wing as a Component of the Configuration of a Commercial Airliner

Anotace: This paper introduces the methodology and the method of automated design of additional aerodynamic surfaces of the wing as a component of the configuration of a commercial airliner, based on the suggested mathematical model. The mathematical model makes it possible to solve a particular task of developing and designing an additional aerodynamic surface of the wing for a commercial airliner and to select the required type of additional aerodynamic surface for a certain aircraft. The decision on the required type of additional aerodynamic surface for a certain aircraft is made using a specialized software product, based on the implementation of a multi-criterial approach to the selection of the method in the process of defining the set tasks. The automation of the design process of additional aerodynamic surfaces of the wing as a component of the configuration of a commercial airliner is achieved by means of the developed software product, written in an objectoriented high-level programming language.