Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/5667
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dc.contributor.authorGürdamar E.-
dc.contributor.authorÇete R.-
dc.contributor.authorAksel H.-
dc.contributor.authorKaynak Ünver-
dc.date.accessioned2021-09-11T15:19:33Z-
dc.date.available2021-09-11T15:19:33Z-
dc.date.issued2006en_US
dc.identifier.citation24th AIAA Applied Aerodynamics Conference, 5 June 2006 through 8 June 2006, San Francisco, CA, 68786en_US
dc.identifier.isbn1563478129; 9781563478123-
dc.identifier.issn1048-5953-
dc.identifier.urihttps://hdl.handle.net/20.500.11851/5667-
dc.description.abstractThe ?-Re?t correlation-based turbulence model is numerically studied using the well-known flat plate transition experiment test cases for better understanding the effect of correlation formulas in the model. Empirical correlations used in the present model are developed by numerical experimentation and the skin-friction coefficients are compared with the ERCOFTAC T3A flat plate test case for the bypass transition regime and the classical Schubauer&Klebanoff for the natural transition regime. It was found that the new correlation values between the transition momentum thickness Reynolds number and the parameter that controls the extent of the transition region displayed good agreement with the experimental data for the T3A and Schubauer&Klebanoff test cases.en_US
dc.language.isoenen_US
dc.relation.ispartofCollection of Technical Papers - AIAA Applied Aerodynamics Conferenceen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.titleDetermination of Transition Correlations for Zero-Pressure Gradient Flat Plate Flowsen_US
dc.typeConference Objecten_US
dc.departmentFaculties, Faculty of Engineering, Department of Mechanical Engineeringen_US
dc.departmentFakülteler, Mühendislik Fakültesi, Makine Mühendisliği Bölümütr_TR
dc.identifier.volume2en_US
dc.identifier.startpage987en_US
dc.identifier.endpage994en_US
dc.identifier.scopus2-s2.0-33845415241en_US
dc.institutionauthorKaynak, Ünver-
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.relation.conference24th AIAA Applied Aerodynamics Conferenceen_US
dc.identifier.scopusquality--
item.openairetypeConference Object-
item.languageiso639-1en-
item.grantfulltextnone-
item.fulltextNo Fulltext-
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.cerifentitytypePublications-
Appears in Collections:Makine Mühendisliği Bölümü / Department of Mechanical Engineering
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
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