The effect of nose shape asymmetries on the aerodynamics of a 10 degree cone (d=5 in) was studied in ARL's 20-in.-hypersonic wind tunnel. Surface pressures were measured at various angles of attack and sideslip. Schlieren pictures were taken with a special nose model at several roll attitudes. Stability derivatives were measured by the free oscillation technique. (Author)


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    Titel :

    Aerodynamics of a Slender Cone with Asymmetric Nose Bluntness at Mach 14


    Beteiligte:
    O. Walchner (Autor:in) / F. M. Sawyer (Autor:in) / K. E. Yelmgren (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    5 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch