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dc.creatorMicković, Dejan
dc.creatorJaramaz, Slobodan
dc.creatorElek, Predrag
dc.creatorJaramaz, Dragana
dc.creatorMicković, Dušan
dc.date.accessioned2022-09-19T17:12:23Z
dc.date.available2022-09-19T17:12:23Z
dc.date.issued2013
dc.identifier.issn0021-8936
dc.identifier.urihttps://machinery.mas.bg.ac.rs/handle/123456789/1717
dc.description.abstractThe determination of pressure profiles behind a projectile has been a subject of investigations for more than 70 years. For lumped parameter models it was especially important to determine the pressure on the projectile base, pressure on the chamber base, and pressure for the propellant burning law. In the paper two analytical methods and one numerical method are considered. The analytical methods of proportionate expansion and two-phase mixture are studied. Pressure profiles are also computed numerically by TWO Phase Interior Ballistics (TWOPIB) code, which is based on the model of two-phase flow of solid propellant and its products of combustion, treated as separate phases with appropriate conservation laws and interactions between phases. Through comparison with experimental results on the real weapon system TWOPIB code showed great advantages over analytical methods.en
dc.publisherASME, New York
dc.relationinfo:eu-repo/grantAgreement/MESTD/Integrated and Interdisciplinary Research (IIR or III)/47029/RS//
dc.rightsrestrictedAccess
dc.sourceJournal of Applied Mechanics-Transactions of The Asme
dc.subjecttwo-phase flow modelen
dc.subjectpropellant chargeen
dc.subjectprojectileen
dc.subjectinterior ballisticsen
dc.titleDetermination of Pressure Profiles Behind Projectiles During Interior Ballistic Cycleen
dc.typearticle
dc.rights.licenseARR
dc.citation.issue3
dc.citation.other80(3): -
dc.citation.rankM22
dc.citation.volume80
dc.identifier.doi10.1115/1.4023312
dc.identifier.scopus2-s2.0-84878078555
dc.identifier.wos000326176200003
dc.type.versionpublishedVersion


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Приказ основних података о документу