Topological and parametric optimization of the airplane wing console

Title	Topological and parametric optimization of the airplane wing console
Authors	P. M. Abrashkin¹ ¹Ulyanovsk state technical university
Annotation	The three-dimensional model of an aircraft wing cantilever is considered. On the basis of the model, a methodology for designing the wing force set using topological and parametric optimization methods is developed. Topological optimization is carried out in the OptiStruct program. A number of force set designs are obtained, and parametric optimization is performed in ANSYS Workbench on the basis of the selected optimal variant.
Keywords	polymer composite materials, aviation industry, topology optimization, parameric optimization, objective fumction, mathematical modeling, optimization
Citation	Abrashkin P. M. ''Topological and parametric optimization of the airplane wing console'' [Electronic resource]. Proceedings of the XVI International scientific conference "Differential equations and their applications in mathematical modeling". (Saransk, July 17-20, 2023). Saransk: SVMO Publ, 2023. - pp. 13-19. Available at: https://conf.svmo.ru/files/2023/papers/paper01.pdf. - Date of access: 03.12.2024.