In the following, high-speed measurements on a swept-back wing are reported. The curves of lift, moment, and drag have been determined up to Mach numbers of M = 0.87, and they are compared to a rectangular wing. Through measurements of the total-head loss behind the wing and through schlieren pictures, an insight into the formation of the compression shock at high Mach numbers has been obtained.


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    Titel :

    High-Speed Measurements on a Swept-Back Wing (Sweepback Angle phi = 35 Deg)


    Beteiligte:
    Goethert, B. (Autor:in)


    Erscheinungsdatum :

    01.03.1947


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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