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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    Title :

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


    Contributors:

    Publication date :

    1967


    Size :

    43 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English