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Experimental Investigation of the Boundary Layer Transition on a Laminar Airfoil Using Infrared Thermography

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F18%3AN0000044" target="_blank" >RIV/00010669:_____/18:N0000044 - isvavai.cz</a>

  • Result on the web

    <a href="https://www.epj-conferences.org/articles/epjconf/abs/2018/15/epjconf_efm2018_02040/epjconf_efm2018_02040.html" target="_blank" >https://www.epj-conferences.org/articles/epjconf/abs/2018/15/epjconf_efm2018_02040/epjconf_efm2018_02040.html</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1051/epjconf/201818002040" target="_blank" >10.1051/epjconf/201818002040</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Experimental Investigation of the Boundary Layer Transition on a Laminar Airfoil Using Infrared Thermography

  • Original language description

    The transition in the boundary layer is investigated using infrared thermography (IRT). The study is carried out on a laminar airfoil in the transonic intermittent in-draft wind tunnel. The transition in the boundary layer is evocated using transition-generator strips of different thicknesses at two Mach numbers: 0.4 and 0.8. The tested transition-generators thickness to boundary layer displacement thickness ratio was from 0.42 to 1.25. The Reynolds number respect to the airfoil chord is: Re = 1.0 – 1.4106. The six cases for different transition-generators thickness ratios were compared. The behaviours of laminar and turbulent boundary layers are discussed. The use of IRT has been proven to be an appropriate tool for detecting the transition of the boundary layer in high-speed wind tunnel testing.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20303 - Thermodynamics

Result continuities

  • Project

    <a href="/en/project/TA04020129" target="_blank" >TA04020129: Investigation of flows in a multi-stage axial turbine stages arrangement</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Others

  • Publication year

    2018

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Article name in the collection

    EPJ Web of Conferences, vol. 180, art. no. 02040

  • ISBN

  • ISSN

    21016275

  • e-ISSN

    2100-014X

  • Number of pages

    7

  • Pages from-to

    nestrankovano

  • Publisher name

    EDP Sciences

  • Place of publication

    Neuveden

  • Event location

    Mikulov

  • Event date

    Nov 21, 2017

  • Type of event by nationality

    EUR - Evropská akce

  • UT code for WoS article

    000454317800041