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

Basit Öğe Kaydı
dc.authoridBalikci, Abdulkadir/0000-0003-2621-1570
dc.authorwosidBalikci, Abdulkadir/ABA-4460-2021
dc.contributor.authorTunceroglu, Cagdas
dc.contributor.authorHasirci, Ugur
dc.contributor.authorMaden, Dincer
dc.contributor.authorBalikci, Abdulkadir
dc.date.accessioned2021-12-01T18:47:51Z
dc.date.available2021-12-01T18:47:51Z
dc.date.issued2020
dc.department[Belirlenecek]en_US
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.en_US
dc.description.sponsorshipScientific and Technological Research Council of Turkey (TUBITAK)Turkiye Bilimsel ve Teknolojik Arastirma Kurumu (TUBITAK) [107E115]en_US
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.)en_US
dc.identifier.doi10.1109/TPS.2020.3020704
dc.identifier.endpage4047en_US
dc.identifier.issn0093-3813
dc.identifier.issn1939-9375
dc.identifier.issue11en_US
dc.identifier.scopus2-s2.0-85096099168en_US
dc.identifier.scopusqualityQ3en_US
dc.identifier.startpage4041en_US
dc.identifier.urihttps://doi.org/10.1109/TPS.2020.3020704
dc.identifier.urihttps://hdl.handle.net/20.500.12684/10393
dc.identifier.volume48en_US
dc.identifier.wosWOS:000589269300041en_US
dc.identifier.wosqualityQ4en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherIeee-Inst Electrical Electronics Engineers Incen_US
dc.relation.ispartofIeee Transactions On Plasma Scienceen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectProjectilesen_US
dc.subjectCoilsen_US
dc.subjectInvertersen_US
dc.subjectInsulated gate bipolar transistorsen_US
dc.subjectForceen_US
dc.subjectCoilgunsen_US
dc.subjectRailgunsen_US
dc.subjectCoilgunsen_US
dc.subjectelectromagnetic launchingen_US
dc.subjectpulse width modulation invertersen_US
dc.subjectBore Projectile Dynamicsen_US
dc.subjectPerformanceen_US
dc.subjectDesignen_US
dc.subjectLilen_US
dc.titleThe Experimental Test Results of a Two-Section Linear Induction Launcheren_US
dc.typeArticleen_US

Dosyalar

Orijinal paket
Listeleniyor 1 - 1 / 1
Küçük Resim Yok
İsim:
10393.pdf
Boyut:
2.92 MB
Biçim:
Adobe Portable Document Format
Açıklama:
Tam Metin / Full Text
İndir

Koleksiyon

WoS İndeksli Yayınlar Koleksiyonu
Scopus İndeksli Yayınlar Koleksiyonu