An aircraft including a single fuselage having a main wing and a horizontal stabilizer airfoil pivotally attached at their centers to the fuselage is described. 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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Oblique-wing supersonic aircraft


    Contributors:

    Publication date :

    1976-07-27


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    RTS-303: Variable Geometry, Oblique Wing Supersonic Aircraft

    A. Antaran / H. Belete / M. Dryzmkowski et al. | NTIS | 1992


    RTJ-303: Variable geometry, oblique wing supersonic aircraft

    Antaran, Albert / Belete, Hailu / Dryzmkowski, Mark et al. | NTRS | 1992


    Design of a small supersonic oblique-wing transport aircraft

    TORENBEEK, EGBERT / VAN DER VELDEN / ALEXANDER J. M. | AIAA | 1989



    Oblique Wing Aircraft

    Torenbeek, Egbert | Wiley | 2020