8 research outputs found

    Hemisphere-cylinder in transonic flow, free-stream Mach number from 0.7 to 1.0

    No full text

    Calculations of Hypersonic Flows Over a Series of Indented Nosetips

    No full text

    Hemisphere-Cylinder in Low Supersonic Flow

    No full text

    Low supersonic flow over hemisphere-cylinder at incidence

    No full text

    Errata: Hemisphere-Cylinder in Transonic Flow, M = 0.7-1.0

    No full text
    corecore