An aircraft is described, having a single fuselage with a main wing and a horizontal stabilizer airfoil pivotally attached at their centers to the fuselage. The pivotal attachments allow the airfoils to be yawed relative to the fuselage for high speed flight, and to be positioned at right angles with respect to the fuselage during takeoff, landing, and low speed flight. The main wing and the horizontal stabilizer are upwardly curved from their center pivotal connections towards their ends to form curvilinear dihedrals.


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    Title :

    Single Wing Supersonic Aircraft


    Contributors:
    R. T. Jones (author)

    Publication date :

    1974


    Size :

    40 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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