The subsonic aerodynamic characteristics of a series of irregular planform wings were studied in wind tunnel tests conducted at M = 0.3 over a range of Reynolds numbers from 1.6 million to 26 million/m. The five basic wing planforms varied from a trapezoidal to a delta shape. Leading edge extensions, added to the basic shape, varied in approximately 5 deg increments from the wing leading edge sweep-back angle to a maximum 80 deg. Most of the tests were conducted using an NACA 0008 airfoil section with grit boundary layer trips. Tests were also conducted using an NACA 0012 airfoil section and an 8% thick wedge. In addition, the effect of free transition (no grit) was investigated. A body was used on all models.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Reynolds Number Effects on the Aerodynamic Characteristics of Irregular Planform Wings at Mach Number 0.3


    Beteiligte:
    R. L. Kruse (Autor:in) / G. H. Lovette (Autor:in) / B. Spencer (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    422 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch