AbstractTo study the characteristics of flow separation and self-excited oscillation of a shock train in a rectangular duct, a simple test case has been conducted and analyzed. The high-speed Schlieren technique and high-frequency pressure measurements have been adopted to collect the data. The experimental results show that there are two separation modes in the duct under M3 incoming condition. The separation mode switch has great effects on the flow effects, such as the pressure distribution, the standard deviation distribution and so on. The separation mode switch can be judged by the history of pressure standard deviation. When it comes to the self-excited oscillation of a shock train, the frequency contents in the undisturbed region, the intermittent region, and the separated bubble have been compared. It was found that the low-frequency disturbance induced by the upstream shock foot motions can travel downstream and the frequency will be magnified by the separation bubble. The oscillation of the small shock foot and the oscillation of the large shock foot are associated with each other rather than oscillating independently.

    HighlightsThe flow separation and self-excited oscillation have been studied experimentally.Two separation modes have been found experimentally in Mach 3 duct flow.The frequency of the upstream disturbance can be magnified by the separation bubble.The oscillation of two separation shock foots are associated with each other.


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    Titel :

    Experimental study on the flow separation and self-excited oscillation phenomenon in a rectangular duct


    Beteiligte:
    Xiong, Bing (Autor:in) / Wang, Zhen-Guo (Autor:in) / Fan, Xiao-Qiang (Autor:in) / Wang, Yi (Autor:in)

    Erschienen in:

    Acta Astronautica ; 133 ; 158-165


    Erscheinungsdatum :

    2017-01-06


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch