Tests conducted on model designed for orbital, probe and re-entry missions, through angle of attack range from -8 to 8° at average test of 4.0×106 Re/ft; variation of peak negative pressures associated with corners at nose and transition flare may cause critical local loading condition to occur at Mach close to 0. 90; effects of adding protuberances presented.


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    Titel :

    Aerodynamic loading characteristics at Mach numbers from 0.80 to 1.20 of 1/10-scale three-stage scout model


    Weitere Titelangaben:

    NASA -- Tech Notes


    Beteiligte:
    Kelly, T.C. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    64 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :