The effects of wing trailing-edge control surfaces on the static transonic aerodynamic characteristics of a transport configuration with a supercritical wing were studied. The configuration was tested with both an area-ruled fuselage and a cylindrical fuselage. The Mach number range was from 0.80 to 0.96 and the angle of attack range was from -1 deg to 12 deg. The Reynolds number was 1,580,000 based on the mean aerodynamic chord. Tabular data are presented.


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    Titel :

    Transonic aerodynamic characteristics of a supercritical-wing transport model with trailing-edge controls


    Beteiligte:
    Mann, M. J. (Autor:in) / Langhans, R. A. (Autor:in)

    Erscheinungsdatum :

    1977-10-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :