In conjunction with an earlier transonic test, a 0.04-scale model of the Saturn V launch vehicle was tested at Mach numbers from 1.80 to 3.00 for Reynolds number based on model diameter varying from 1.59 to 2.77 million. Static pressure distributions and boundary-layer profiles were measured and are presented herein.


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    Titel :

    Pressure Test on a 0.04-Scale Model of the Saturn V Launch Vehicle at Mach Numbers from 1.80 Through 3.00


    Beteiligte:
    T. R. Brice (Autor:in) / J. E. Robertson (Autor:in)

    Erscheinungsdatum :

    1967


    Format / Umfang :

    43 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch