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dc.contributor.authorCengizci, Süleyman
dc.date.accessioned2020-01-03T07:41:37Z
dc.date.available2020-01-03T07:41:37Z
dc.date.issued2019
dc.identifier.citationCengizci, S. (2019). One-dimensional finite element simulations for chemically reactive hypersonic flows. 8th International Eurasian Conference on Mathematical Sciences and Applications (IECMSA-2019), Baku.en_US
dc.identifier.urihttp://hdl.handle.net/20.500.12566/226
dc.descriptionInternational Eurasian Conference on Mathematical Sciences and Applications (8. : 2019 : Baku, Azerbaijan)
dc.description.abstractHypersonic vehicles are utilized in recent years massively for both military and civilian purposes. As the vehicles fly through an atmosphere at hypersonic speeds (generally considered as Mach>), they experience critical physical and chemical interactions due to extremely high (several thousands of Kelvin) temperatures generated around the vehicles. This high-temperature effects may cause vibrational excitation, dissociation and ionization of atoms and molecules. Therefore, the perfect gas hypothesis is no longer valid for air and high temperature effects also should be included in the mathematical model. Hypersonic vehicles are utilized in recent years massively for both military and civilian purposes. As the vehicles fly through an atmosphere at hypersonic speeds (generally considered as M ach > 5), they experience critical physical and chemical interactions due to extremely high (several thousands of Kelvin) temperatures generated around the vehicles. This high-temperature effects may cause vibrational excitation, dissociation and ionization of atoms and molecules. Therefore, the perfect gas hypothesis is no longer valid for air and high temperature effects also should be included in the mathematical model. In this study, one-dimensional compressible multi-species Navier-Stokes Equations for thermochemical non-equilibrium are simulated utilizing a Galerkin Finite Element Method. Air mixture is considered as a combination of atoms Oxygen (O), Nitrogen (N) and molecules Nitric oxide (NO), Dioxygen (O2), Dinitrogen (N2).en_US
dc.description.sponsorshipNo sponsoren_US
dc.language.isoengen_US
dc.publisher8th International Eurasian Conference on Mathematical Sciences and Applications (IECMSA-2019)en_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectHypersonicen_US
dc.subjectHipersoniktr_TR
dc.subjectNon-equilibrium flowen_US
dc.subjectDenge dışı akıştr_TR
dc.subjectChemically reactiveen_US
dc.subjectKimyasal olarak reaktiftr_TR
dc.subjectFinite elementen_US
dc.subjectSonlu elemanlartr_TR
dc.subjectVibration-dissociation couplingen_US
dc.subjectTitreşim ayrıştırma bağlantısıtr_TR
dc.titleOne-dimensional finite element simulations for chemically reactive hypersonic flowsen_US
dc.typeinfo:eu-repo/semantics/conferenceObjecten_US
dc.relation.publicationcategoryInternational publicationen_US
dc.contributor.orcid0000-0002-4345-1253 [Cengizci, Süleyman]
dc.contributor.abuauthorCengizci, Süleyman
dc.contributor.yokid215405 [Cengizci, Süleyman]


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