Title | Topological and parametric optimization of the airplane wing console |
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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: 04.12.2024. |
© SVMO, National Research Mordovia State University, 2024
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