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METHOD OF DETERMINATION OF RATIONAL DESIGN PARAMETERS USING THE FINITE-ELEMENT METHOD

巻 46, 発行 2, 2015, pp. 175-192
DOI: 10.1615/TsAGISciJ.2015014219
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要約

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.

によって引用された
  1. 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

  2. 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

  3. 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

  4. 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

  5. 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

  6. 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

  7. 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

最新号

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