Attention is directed to the acoustics research of the 1950s and 1960s for guidance in understanding and quantizing the turbulence amplification that can occur in regions of shock-wave boundary-layer interaction. Three primary turbulence amplifier-generator mechanisms are identified and shown, by linear analysis, to be responsible for turbulence amplification across a shock wave in excess of 100% of the incident turbulence intensity.


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    Titel :

    Turbulence amplification in shock-wave boundary-layer interaction


    Beteiligte:
    Anyiwo, J. C. (Autor:in) / Bushnell, D. M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1982-07-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :