The aerodynamic configuration of a vertical takeoff transport aircraft with fan lift propulsion system is discussed. Specifications of the geometry, inertia, and aerodynamic characteristics are presented. The composition and performance of the propulsion system are analyzed. Tables of data are included to show dimensions and predicted performance.


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    Titel :

    Aircraft Design Studies Vertical Take off and Landing Airliner


    Beteiligte:
    D. Howe (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    53 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch