This paper presents the design and the results of the qualification test campaign of a multiple Mach number supersonic wind tunnel designed for induced boundary layer transition. Its characteristics, function, and instrumentation are described. The range of Mach numbers successfully span is presented along with the measured intensities of freestream fluctuations. All the measurement techniques implemented in the test campaigns after the qualification are introduced, and some results shown and commented to highlight their potentialities.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Design and qualification of a supersonic wind tunnel for induced boundary layer transition research


    Beteiligte:
    Bottini, H (Autor:in) / Paniagua, G (Autor:in) / Schreivogel, P (Autor:in) / Sonda, A (Autor:in) / de las Heras, S (Autor:in)


    Erscheinungsdatum :

    01.03.2015


    Format / Umfang :

    17 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch