Dr. R. T. Jones first developed the theory for oblique wing aircraft in 1952, and in subsequent years numerous analytical and experimental projects conducted at NASA Ames and elsewhere have established that the Jones' oblique wing theory is correct. Until the late 1980's all proposed oblique wing configurations were wing/body aircraft with the wing mounted on a pivot. With the emerging requirement for commercial transports with very large payloads, 450-800 passengers, Jones proposed a supersonic oblique flying wing in 1988. For such an aircraft all payload, fuel, and systems are carried within the wing, and the wing is designed with a variable sweep to maintain a fixed subsonic normal Mach number. Engines and vertical tails are mounted on pivots supported from the primary structure of the wing. The oblique flying wing transport has come to be known as the Oblique All-Wing (OAW) transport. This presentation gives the highlights of the OAW project that was to study the total concept of the OAW as a commercial transport.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Large Capacity Oblique All-Wing Transport Aircraft


    Beteiligte:
    T. L. Galloway (Autor:in) / J. A. Phillips (Autor:in) / R. A. Kennelly (Autor:in) / M. H. Waters (Autor:in)

    Erscheinungsdatum :

    1996


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Large capacity oblique all-wing transport aircraft

    Galloway, Thomas L. / Phillips, James A. / Kennelly, Robert A., Jr. et al. | NTRS | 1996


    Oblique Wing Aircraft

    Torenbeek, Egbert | Wiley | 2020


    Oblique-wing supersonic aircraft

    Jones, R. T. | NTRS | 1976


    OBLIQUE ROTOR-WING AIRCRAFT

    COMBS CORY MICHAEL | Europäisches Patentamt | 2018

    Freier Zugriff

    Oblique rotor-wing aircraft

    COMBS CORY MICHAEL | Europäisches Patentamt | 2019

    Freier Zugriff