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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    Title :

    Aircraft Design Studies Vertical Take off and Landing Airliner


    Contributors:
    D. Howe (author)

    Publication date :

    1972


    Size :

    53 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English