The lift, drag, and pitching moment of a missile body with boattailing were measured at Mach numbers from 0.5 to 1.0 at a Reynolds number of 340,000 in a transonic wind tunnel. Lift, drag, and longitudinal stability of the body was found to decrease when the relative base diameter decreased.


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    Titel :

    Lift, Drag and Pitching Moment Measurements on a Missile Body Having Various Boattails at Subsonic and Transonic Velocities


    Beteiligte:
    M. Tanner (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    86 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch