EXTRUSION FORMING OF A DOUBLE BASE SOLID ROCKET PROPELLANT BY FINITE ELEMENT METHOD

dc.authoriddirikolu, m. husnu/0000-0001-6279-2283
dc.contributor.authorKalaycioglu, Baris
dc.contributor.authorDirikolu, M. Husnu
dc.contributor.authorCelik, Veli
dc.date.accessioned2025-01-21T16:41:08Z
dc.date.available2025-01-21T16:41:08Z
dc.date.issued2007
dc.departmentKırıkkale Üniversitesi
dc.description.abstractIn this study, three dimensional modelling of extrusion forming of a double base solid rocket propellant is performed on Ansys (R) finite element simulation package. For the purpose of initial model construction and later comparisons with elastoviscoplastik model, the solid propellant is assumed to obey the elastic-plastic material response during the direct extrusion process. Taking into account the contact surface behavior with Coulomb friction and geometric and material nonlinearities, an incremental large large strain solution methodology has been adapted in the simulation. The hydrostatic pressure, stress, strain, and displacement values during extrusion of the solid rocket propellant are obtained from the simulation.
dc.identifier.endpage37
dc.identifier.issn1300-7009
dc.identifier.issn2147-5881
dc.identifier.issue1
dc.identifier.startpage31
dc.identifier.urihttps://hdl.handle.net/20.500.12587/24810
dc.identifier.volume13
dc.identifier.wosWOS:000443126900005
dc.identifier.wosqualityN/A
dc.indekslendigikaynakWeb of Science
dc.language.isotr
dc.publisherPamukkale Univ
dc.relation.ispartofPamukkale University Journal of Engineering Sciences-Pamukkale Universitesi Muhendislik Bilimleri Dergisi
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_20241229
dc.subjectDouble base solid rocket propellant; Direct extrusion; Finite element method; Elastic-plastic
dc.titleEXTRUSION FORMING OF A DOUBLE BASE SOLID ROCKET PROPELLANT BY FINITE ELEMENT METHOD
dc.typeArticle

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