Приказ основних података о документу

dc.creatorElek, Predrag
dc.creatorJaramaz, Slobodan
dc.creatorMicković, Dejan
dc.date.accessioned2023-03-02T10:15:18Z
dc.date.available2023-03-02T10:15:18Z
dc.date.issued2012
dc.identifier.isbn978-86-81123-58-4
dc.identifier.urihttps://machinery.mas.bg.ac.rs/handle/123456789/4894
dc.description.abstractThe paper considers acceleration of cylindrical metal liner by expanding detonation products. A new analytical model of liner motion is developed for the cases of axisymmetric (head-on) and grazing (side-on) detonation of the explosive charge. Suggested model relies on the two-stage regime of cylinder motion: (i) the first stage is the consequence of detonation wave-metallic liner interaction; as the result initial velocity is imparted to the liner, (ii) the second stage is gas-dynamic push of the liner governed by detonation product expansion, similarly to the Gurney approach. Results of the analytical model are validated by comparison with available experimental data.sr
dc.language.isoensr
dc.publisherBelgrade : Military Technical Institutesr
dc.relationinfo:eu-repo/grantAgreement/MESTD/Integrated and Interdisciplinary Research (IIR or III)/47029/RS//sr
dc.rightsopenAccesssr
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.source5th International Scientific Conference on Defensive Technologies – OTEH 2012sr
dc.subjectexplosive propulsionsr
dc.subjectdetonationsr
dc.subjectshock wavessr
dc.subjectplasticitysr
dc.subjectanalytical modelsr
dc.titleTwo-stage model of explosive propulsion of metal cylindersr
dc.typeconferenceObjectsr
dc.rights.licenseBYsr
dc.citation.epage300
dc.citation.spage294
dc.identifier.fulltexthttp://machinery.mas.bg.ac.rs/bitstream/id/11944/3-21.pdf
dc.identifier.rcubhttps://hdl.handle.net/21.15107/rcub_machinery_4894
dc.type.versionpublishedVersionsr


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Приказ основних података о документу