Please use this identifier to cite or link to this item: https://repository.hneu.edu.ua/handle/123456789/24549
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dc.contributor.authorMisura S. I.-
dc.contributor.authorPodgorny A.-
dc.contributor.authorSmetankina N. V.-
dc.contributor.authorMisiura Ie. Iu.-
dc.date.accessioned2021-02-04T09:56:23Z-
dc.date.available2021-02-04T09:56:23Z-
dc.date.issued2020-
dc.identifier.citationMisiura S. Rational Design of the Cyclically Symmetrical Structure / S. Misura, A. Podgorny, N. Smetankina, Ie. Misiura // Integrated Computer Technologies in Mechanical Engineering” ICTM-2020 : міжнар. науково-практ. конф. : тези допов. – Харків : Нац. аерокосм. ун-т ім. М. Є. Жуковського «Харків. авіац. ін-т», 2020. – P. 7–10.ru_RU
dc.identifier.urihttp://repository.hneu.edu.ua/handle/123456789/24549-
dc.description.abstractThe problem of optimal design of a Kaplan turbine cover operating in the normal mode is solved. The geometric parameters of the cover are modified to minimize the cover weight. To calculate the parameters of the strain-stress state, the finite element method is used. Optimization was performed using the gradient method. The design variables are the thicknesses of structural elements. The weight of the cover was reduced by 30 %, and the rolled stock thickness range was downsized by five positions. In this case, the stress values in the optimal structure did not exceed admissible ones.ru_RU
dc.language.isoenru_RU
dc.subjectoptimizationru_RU
dc.subjectKaplan turbineru_RU
dc.subjectstrain-stress stateru_RU
dc.subjectgradient methodru_RU
dc.titleRational Design of the Cyclically Symmetrical Structureru_RU
dc.typeArticleru_RU
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