Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/11577
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dc.contributor.authorРодченко, Олександр Васильович-
dc.date.accessioned2014-11-09T17:07:28Z-
dc.date.available2014-11-09T17:07:28Z-
dc.date.issued2014-05-08-
dc.identifier.citationImprovement of the two-layer airfield rigid pavement design / O. V. Rodchenko // 17th Conference of Young Scientists of Lithuania „Science – Lithuania‘s Future. TRANSPORT“, 8th of May 2014: Proceedings. – Vilnius, 2014. – Р. 32-36.-
dc.identifier.isbn978-609-457-714-7-
dc.identifier.issn2029-7157-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/11577-
dc.description.abstractThe State norms of Ukraine have only two values of transition factor (one value for free-edge loading case, other for joint edge) which do not allow aircraft main landing gear and number of wheels. Transition factors for calculation of edge bending moment are determined for airfield rigid pavement design. New values of transition factors account main landing gear configuration of new aircrafts. Transition factor values are obtained by using finite element modeling programs LIRA and FEAFAA.uk_UA
dc.language.isoenuk_UA
dc.publisherTRANSPORT ENGINEERING AND MANAGEMENT, 8 May 2014, Vilnius, Lithuaniauk_UA
dc.subjectairfield rigid pavementuk_UA
dc.subjectmain landing gearuk_UA
dc.subjectdowel baruk_UA
dc.subjectjointuk_UA
dc.subjecttransition factoruk_UA
dc.subjectdeflectionuk_UA
dc.subjectstrainuk_UA
dc.subjectjoint load transfer efficiencyuk_UA
dc.subjectfinite element modelinguk_UA
dc.titleIMPROVEMENT OF THE TWO-LAYER AIRFIELD RIGID PAVEMENT DESIGNuk_UA
dc.typeArticleuk_UA
dc.specialityБудівництвоuk_UA
Appears in Collections:Наукові статті кафедри комп'ютерних технологій будівництва (архів)

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