The Experimental Test Results of a Two-Section Linear Induction Launcher

dc.contributor.authorTunceroglu, Cagdas
dc.contributor.authorHasirci, Ugur
dc.contributor.authorMaden, Dincer
dc.contributor.authorBalıkçı, Abdulkadir
dc.date.accessioned2025-10-29T11:13:55Z
dc.date.issued2020
dc.departmentFakülteler, Mühendislik Fakültesi, Elektronik Mühendisliği Bölümü
dc.description.abstractA linear induction launcher (LIL) is an air-cored coilgun. Its barrel consists of an array of cylindrical drive coils and the barrel can be a single section or divided into several sections. A single-section barrel can be easily driven by energizing the coils in a polyphase fashion to accelerate the moving part of the LIL, the projectile. A multisection barrel, on the other hand, offers higher muzzle velocities for the projectile. From breech to muzzle, each section is energized with an increasing frequency. However, several problems arise when a multisection barrel is used. Some of them are currently reported in the literature. For example, a retarding force on the projectile has been observed while the projectile passes from one section to another. The initial position of the projectile also affects the launching performance. Some experiments can be useful to determine the optimum conditions to reach maximum possible muzzle velocity. This article concerns the design, implementation, and experimental test of a laboratory-scale, two-section LIL to examine the effects of various parameters on the launching performance.
dc.description.sponsorshipScientific and Technological Research Council of Turkey (TUBITAK) [107E115]
dc.description.sponsorshipThis work was supported by the Scientific and Technological Research Council of Turkey (TUBITAK) under Grant 107E115. The review of this article was arranged by Senior Editor D. A. Wetz. (Corresponding author: Ugur Hasirci.)
dc.identifier.doi10.1109/TPS.2020.3020704
dc.identifier.endpage4047
dc.identifier.issn0093-3813
dc.identifier.issn1939-9375
dc.identifier.issue11
dc.identifier.orcid0000-0003-2621-1570
dc.identifier.orcid0000-0001-5419-5083
dc.identifier.orcid0000-0001-8503-7694
dc.identifier.scopus2-s2.0-85096099168
dc.identifier.scopusqualityQ2
dc.identifier.startpage4041
dc.identifier.urihttps://doi.org/10.1109/TPS.2020.3020704
dc.identifier.urihttps://hdl.handle.net/20.500.14854/6971
dc.identifier.volume48
dc.identifier.wosWOS:000589269300041
dc.identifier.wosqualityQ4
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherIEEE-Inst Electrical Electronics Engineers Inc
dc.relation.ispartofIEEE Transactions on Plasma Science
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.snmzKA_WOS_20251020
dc.subjectProjectiles
dc.subjectCoils
dc.subjectInverters
dc.subjectInsulated gate bipolar transistors
dc.subjectForce
dc.subjectCoilguns
dc.subjectRailguns
dc.subjectCoilguns
dc.subjectelectromagnetic launching
dc.subjectpulse width modulation inverters
dc.titleThe Experimental Test Results of a Two-Section Linear Induction Launcher
dc.typeArticle

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