Technique for relating transient tolerances in inlet throat Mach number and shock position to supersonic unstart frequency due to atmospheric turbulence for supersonic inlet design


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    Titel :

    Development of atmospheric gust criteria for supersonic inlet design


    Beteiligte:
    Barry, F. W. (Autor:in)

    Erscheinungsdatum :

    01.12.1968


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



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