Finite element analysis of dynamic responses for honeycomb sandwich plates initially damaged by skin/core partial debonding

dc.contributor.authorBurlayenko, Vyacheslav. N.en
dc.contributor.authorSadowski, Tomaszen
dc.date.accessioned2021-02-10T09:05:02Z
dc.date.available2021-02-10T09:05:02Z
dc.date.issued2008
dc.identifier.citationBurlayenko V. N. Finite element analysis of dynamic responses for honeycomb sandwich plates initially damaged by skin/core partial debonding / V. N. Burlayenko, T. Sadowski // 8th World Congress on Computational Mechanics (WCCM8), 5th European Congress on Computational Methods in Applied Sciences and Engineeering (ECCOMAS 2008), June 30-July 5, 2008, Venice, Italy : bk. of abstr. / eds.: B. A. Schrefler, U. Perego ; Intern. Center for Numerical Methods in Engineering. – Spain : Artes Graficas Torres S. L., 2008. – 2 p.en
dc.identifier.urihttps://repository.kpi.kharkov.ua/handle/KhPI-Press/50913
dc.language.isoen
dc.publisherArtes Graficas Torres S. L., Spainen
dc.subjectdynamic analysisen
dc.subjectdebondingen
dc.subjecthoneycomb sandwich platesen
dc.subjectfinite element predictionsen
dc.titleFinite element analysis of dynamic responses for honeycomb sandwich plates initially damaged by skin/core partial debondingen
dc.typeThesisen

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