Experimental aerodynamic investigations were conducted at the CALSPAN Corporation's transonic wind tunnel to determine the aerodynamic characteristics of several nose-mounted canard wing configurations. Canard position, geometry, angular orientation, and model nose shape were varied systematically to determine their effects on model aerodynamics. Angle of attack was varied from -3 to 12 degrees and Mach number was varied from 0.6 to 1.25. Aerodynamic loads were measured separately for each of the four canards and tail surfaces, and the total model.


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    Titel :

    An Experimental Investigation of the Aerodynamic Characteristics of Several Nose-Mounted Canard Configurations at Transonic MACH Numbers


    Beteiligte:
    J. R. Burt (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    779 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch