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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    Title :

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


    Additional title:

    NASA -- Tech Notes


    Contributors:
    Kelly, T.C. (author)


    Publication date :

    1961


    Size :

    64 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English