Publicado 6 números por año
ISSN Imprimir: 1948-2590
ISSN En Línea: 1948-2604
METHOD OF DETERMINATION OF RATIONAL DESIGN PARAMETERS USING THE FINITE-ELEMENT METHOD
SINOPSIS
The article discusses the technique of carrying out design calculations of wings made of composite materials. Reviewed are the calculation results of some rational parameters of thin-walled structures elements under the influence of aerodynamic forces.
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Korchagin P. A, Letopolskiy A. B., Teterina I. A., RESEARCH RESULTS OF THE EFFICIENCY OF THE MOTOR GRADER SIDE WORKING EQUIPMENT, Vestnik SibADI, 15, 4, 2018. Crossref
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Berezhnoi D V, Antonova E V, Balafendieva I S, Vildanova N R, Miheev V V, Sekaeva L R, Investigation of nonlinear deformation of solid and porous elements of three-dimensional structures, Journal of Physics: Conference Series, 1158, 2019. Crossref
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Berezhnoi D V, Shamim M R, Balafendieva I S, Kasumov E V, Sekaeva L R, Fakhrutdinov L R, Numerical investigation for process of deformation of a multilayer shell under thermal loading, Journal of Physics: Conference Series, 1158, 2019. Crossref
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Kasumov E V, Berezhnoi D V, Numerical modeling of the dynamics of the mechanical system from composition materials, Journal of Physics: Conference Series, 1158, 2019. Crossref
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Tatarnikov O.V., Phyo W.A., Naing Lin Aung, Multi-Criteria Optimization of a Two-Spar Composite Wing for a Light Aircraft, Proceedings of Higher Educational Institutions. Маchine Building, 5 (734), 2021. Crossref
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Balafendieva I S, Galimullin I A, Bajtemirov I K, Numerical study of non-linear deformation processes of porous concrete, IOP Conference Series: Materials Science and Engineering, 709, 4, 2020. Crossref
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Baranovski S V, Mikhailovskiy K V, Selection and justification of polymer composite wing load-bearing elements design parameters with material anisotropy and airload, IOP Conference Series: Materials Science and Engineering, 934, 1, 2020. Crossref