This paper presents a novel experimental technique where infrared thermography is employed to directly measure the surface heat transfer of a transpiration-cooled porous material in transient hypersonic flow. Experiments were conducted in the Oxford High Density Tunnel on a flat-faced hemispherical probe at a single Mach 7 freestream condition ( R e u = 3.84 10 6    m 1 ) with nitrogen, air, argon, krypton, and helium injection gases and mass flow rates ranging from 0.01 to 0.235    kg s 1 m 2 . Surface heat transfer measurements were extracted by imaging directly on the porous material using a FLIR A6751 high-speed long-wave infrared camera. Porous alumina was chosen due to its favorable thermal properties for infrared analysis and its very small pore sizes ( 2    μ m ) enabling a uniform outflow. It was found that the surface Stanton number reduction matched to within 10% of both computational fluid dynamics results and correlations.


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    Titel :

    Heat Transfer Measurements of a Transpiration-Cooled Stagnation Point in Transient Hypersonic Flow


    Beteiligte:
    Naved, Imran (Autor:in) / Hermann, Tobias (Autor:in) / McGilvray, Matthew (Autor:in) / Ewenz Rocher, Marc (Autor:in) / Hambidge, Chris (Autor:in) / Doherty, Luke (Autor:in) / Le Page, Laurent (Autor:in) / Grossman, Madeleine (Autor:in) / Vandeperre, Luc (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2022-09-02


    Format / Umfang :

    13 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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