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dc.contributor.authorDundar, Furkan Semih
dc.date.accessioned2024-03-12T19:28:50Z
dc.date.available2024-03-12T19:28:50Z
dc.date.issued2022
dc.identifier.issn0188-7009
dc.identifier.issn1661-4909
dc.identifier.urihttps://doi.org/10.1007/s00006-022-01208-0
dc.identifier.urihttps://hdl.handle.net/20.500.12450/2065
dc.description.abstractIn this study, we used the fact that unit circle for elliptic numbers is an ellipse to model motion of a planet around a star. For that purpose we first have given a standard derivation of elliptic orbits in Newtonian two-body problem. Then we translated the variables found in the coordinates where the origin is at the focus of the ellipse to elliptic number parameters where the origin is at the center of the ellipse. We noted that a similar argument may be used to model hyperbolic orbits in Newtonian gravity with hyperbolic numbers. However it seems that modelling parabolic orbits is not possible within the context of p-complex numbers.en_US
dc.language.isoengen_US
dc.publisherSpringer Basel Agen_US
dc.relation.ispartofAdvances In Applied Clifford Algebrasen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectp-Complex numbersen_US
dc.subjectClifford Algebraen_US
dc.subjectTwo body problemen_US
dc.subjectNewtonian gravityen_US
dc.titleA Use of Elliptic Complex Numbers in Newtonian Gravityen_US
dc.typearticleen_US
dc.departmentAmasya Üniversitesien_US
dc.identifier.volume32en_US
dc.identifier.issue2en_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.identifier.scopus2-s2.0-85125452948en_US
dc.identifier.doi10.1007/s00006-022-01208-0
dc.department-temp[Dundar, Furkan Semih] Amasya Univ, Dept Mech Engn, TR-05100 Amasya, Turkeyen_US
dc.identifier.wosWOS:000758827300002en_US


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