- Lift measurement of airfoil AH93-157 from wall pressure distribution
Number of the records: 1  

Lift measurement of airfoil AH93-157 from wall pressure distribution

  1. 1.
    SYSNO ASEP0559030
    Document TypeC - Proceedings Paper (int. conf.)
    R&D Document TypeThe record was not marked in the RIV
    TitleLift measurement of airfoil AH93-157 from wall pressure distribution
    Author(s) Procházka, Pavel P. (UT-L) RID, ORCID, SAI
    Skála, Vladislav (UT-L) ORCID
    Antoš, Pavel (UT-L) RID, ORCID
    Popelka, L. (CZ)
    Fürst, J. (CZ)
    Schmirler, M. (CZ)
    Article number01031
    Source TitleEPJ Web of Conferences, EFM21 – 15th International Conference Experimental Fluid Mechanics 2021, 264. - Cedex A : EDP Sciences, 2022
    Number of pages4 s.
    Publication formOnline - E
    ActionEFM21 – International Conference Experimental Fluid Mechanics 2021 /15./
    Event date23.11.2021 - 26.11.2021
    VEvent locationLiberec
    CountryCZ - Czech Republic
    Event typeWRD
    Languageeng - English
    CountryFR - France
    Keywordslift coefficient ; pressure distribution ; airfoil
    Subject RIVBK - Fluid Dynamics
    OECD categoryApplied mechanics
    R&D ProjectsGA20-26779S GA ČR - Czech Science Foundation (CSF)
    Institutional supportUT-L - RVO:61388998
    DOI https://doi.org/10.1051/epjconf/202226401031
    AnnotationMeasurement of the lift coefficient of the AH93-157 airfoil was performed by measuring the static pressure distribution on the wind tunnel walls along the test-section. A correlation was established between the lift coefficient value, determined by integrating the static pressure distribution on the wind tunnel walls, and the lift coefficient value, determined by integrating the static pressure distribution on the airfoil surface. This method is useful for easy and quick determination of the lift coefficient on a simple airfoil model without complicated static pressure tubing from the surface. The measurement was made within a closed test-section. The correlation relationship also eliminates the problem of the finite span and the effect of the side walls. Comparison of pressure distribution on airfoil with CFD was performed as well.
    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 Publishing2024
    Electronic addresshttps://www.epj-conferences.org/articles/epjconf/pdf/2022/08/epjconf_efm2022_01031.pdf
Number of the records: 1  

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