Test Simulations with the NACA 0012 Airfoil

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dc.contributorAalto-yliopistofi
dc.contributorAalto Universityen
dc.contributor.authorAla-Juusela, Juhaveikko
dc.contributor.departmentSovelletun termodynamiikan laboratoriofi
dc.contributor.departmentLaboratory of Applied Thermodynamicsen
dc.contributor.schoolTeknillinen korkeakoulufi
dc.contributor.schoolHelsinki University of Technologyen
dc.date.accessioned2016-12-13T10:02:28Z
dc.date.available2016-12-13T10:02:28Z
dc.date.issued2003
dc.descriptionMEMO No CFD/THERMO-44-2003 Date: 17th December 2003
dc.description.abstractAbstract: Air-flow around the NACA 0012 airfoil was simulated with the FINFLO flow solver version 7.2 of Finflo Ltd. and the 2D solver FINF2D of Laboratory of Aerodynamics, HUT. The flow conditions are Ma = 0.3, α = 10°. Main result: Pressure and friction coefficients are in a good agreement between the two solvers, whereas the drag and lift coefficients have some differencies.en
dc.format.extent21
dc.format.mimetypeapplication/pdfen
dc.identifier.urihttps://aaltodoc.aalto.fi/handle/123456789/23727
dc.identifier.urnURN:NBN:fi:aalto-201612135908
dc.language.isoenen
dc.publisherAalto Universityen
dc.publisherAalto-yliopistofi
dc.subject.keywordFINFLOen
dc.subject.keywordk-ω modelen
dc.subject.keywordk-ε modelen
dc.subject.keywordNACA 0012 Airfoilen
dc.subject.otherMechanical engineeringen
dc.titleTest Simulations with the NACA 0012 Airfoilen
dc.typeJ Muu elektroninen julkaisufi
dc.type.dcmitypetexten
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