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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Oblique-wing supersonic aircraft


    Beteiligte:
    Jones, R. T. (Autor:in)

    Erscheinungsdatum :

    27.07.1976


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    RTJ-303: Variable geometry, oblique wing supersonic aircraft

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


    RTS-303: Variable Geometry, Oblique Wing Supersonic Aircraft

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


    Design of a small supersonic oblique-wing transport aircraft

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



    Oblique wing supersonic transport concepts

    Galloway, Thomas / Gelhausen, Paul / Moore, Mark et al. | NTRS | 1992