Number of the records: 1  

Numerical and experimental modelling of transition in a separated boundary layer on the NACA63A421 airfoil

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    SYSNO ASEP0353754
    Document TypeK - Proceedings Paper (Czech conf.)
    R&D Document TypeThe record was not marked in the RIV
    TitleNumerical and experimental modelling of transition in a separated boundary layer on the NACA63A421 airfoil
    Author(s) Ďuriš, M. (CZ)
    Popelka, Lukáš (UT-L)
    Příhoda, Jaromír (UT-L) RID, ORCID
    Šimurda, David (UT-L) RID, ORCID
    Number of authors4
    Source TitleHYDRO/TERMO – XXIX. setkání kateder mechaniky tekutin a termomechaniky. - Ostrava : VŠB- Technická univerzita Ostrava, 2010 / Dvořák L. ; Fojtášek K. ; Krutil J. ; Zavadil L. - ISBN 978-80-248-2244-0
    S. 45-48
    Number of pages4 s.
    Publication formCD-ROM - CD-ROM
    ActionSetkání kateder mechaniky tekutin a termomechaniky /29./
    Event date23.06.2010-25.06.2010
    VEvent locationRožnov pod Radhoštěm
    CountryCZ - Czech Republic
    Event typeEUR
    Languageeng - English
    CountryCZ - Czech Republic
    Keywordslaminar separated bubble ; transition modelling
    Subject RIVBK - Fluid Dynamics
    R&D Projects1M06031 GA MŠMT - Ministry of Education, Youth and Sports (MEYS)
    GA103/09/0977 GA ČR - Czech Science Foundation (CSF)
    CEZAV0Z20760514 - UT-L (2005-2011)
    AnnotationThe paper is concerned with numerical modelling of transition in a separated boundary layer. A transition model is based on the combination of empirical terms determining position of the transition and averaged Navier–Stokes equations closed by SST turbulence model. The model of transition is applied in computation of 2D flow past NACA63A421 airfoil. Computation is performed using commercial code Fluent 6.3.26, in which the transition model is implemented as a User-Defined-Function. Computed distributions of the pressure coefficient along the airfoil are verified by comparison with experimental data, which were obtained by measurements in a closed circuit wind tunnel at the constant Reynolds number and several angles of attack. The comparison proves the applicability of the implemented transition model.
    WorkplaceInstitute of Thermomechanics
    ContactMarie Kajprová, kajprova@it.cas.cz, Tel.: 266 053 154 ; Jana Lahovská, jaja@it.cas.cz, Tel.: 266 053 823
    Year of Publishing2011
Number of the records: 1  

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