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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    Title :

    Transonic Aerodynamic Characteristics of a Supercritical-Wing Transport Model with Trailing-Edge Controls


    Contributors:
    M. J. Mann (author) / R. A. Langhans (author)

    Publication date :

    1977


    Size :

    336 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English