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dc.contributor.authorHuang, Chi-Chenen_US
dc.contributor.authorHung, Chinghuaen_US
dc.contributor.authorHung, Jung-Chungen_US
dc.contributor.authorLin, Chia-Rungen_US
dc.date.accessioned2019-04-02T06:04:34Z-
dc.date.available2019-04-02T06:04:34Z-
dc.date.issued2012-01-01en_US
dc.identifier.issn1660-9336en_US
dc.identifier.urihttp://dx.doi.org/10.4028/www.scientific.net/AMM.110-116.2708en_US
dc.identifier.urihttp://hdl.handle.net/11536/150557-
dc.description.abstractThe aim of this research is to investigate numerically the neck-spinning process of a tube at elevated temperature. The commercial software Abaqus/Explicit was adopted in the simulation. For the construction of the material model, special uni-axial tensile tests were conducted at elevated temperature and various strain rates, since the material is sensitive to strain rates at high temperature. The influence of the element type and mass scaling factor were investigated through numerical simulation. Full-integration shell element is the better choice in the simulation of the neck-spinning process at elevated temperature. The use of suitable mass scaling factor will make the analysis more efficiency. Comparisons between experimental and simulation results on thickness distribution and the outer contour of the spun tube are discussed. Good agreement was found between experimental and simulation results.en_US
dc.language.isoen_USen_US
dc.subjectcomponenten_US
dc.subjectfinite element analysisen_US
dc.subjecthot neck-spinningen_US
dc.subjectstrain rateen_US
dc.subjectmass scaling factoren_US
dc.subjectelement typeen_US
dc.titleThree Dimension Finite Element Model for Neck-spinning Process of Tube at Elevated Temperatureen_US
dc.typeProceedings Paperen_US
dc.identifier.doi10.4028/www.scientific.net/AMM.110-116.2708en_US
dc.identifier.journalMECHANICAL AND AEROSPACE ENGINEERING, PTS 1-7en_US
dc.citation.volume110-116en_US
dc.citation.spage2708en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:000303370301177en_US
dc.citation.woscount0en_US
Appears in Collections:Conferences Paper