A two-engine, three-fan V/STOL airplane was designed to fulfill naval operational missions. Use of interconnected variable pitch fans led to a good balance between the requirements for high thrust and responsive control at low speed, and efficient thrust at cruise speeds. Engine-out requirements, integration of propulsion and aerodynamic controls, and the propulsion installation were the major factors influencing the configuration. An airplane with a multimission capability from both vertical and short takeoff was conceived.


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    Titel :

    Mechanically coupled lift fan propulsion and control for multimission V/STOL aircraft


    Beteiligte:
    Zabinsky, J. M. (Autor:in) / Gotlieb, P. (Autor:in) / Jakubowski, G. W. (Autor:in)

    Kongress:

    National Aerospace Engineering and Manufacturing Meeting ; 1975 ; Culver City, CA


    Erscheinungsdatum :

    01.11.1975


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Mechanically Coupled Lift Fan Propulsion and Control for Multimission V/STOL Aircraft

    Jakubowski, G. W. / Zabinsky, J. M. / Gotlieb, P. | SAE Technical Papers | 1975




    LIFT FAN PROPULSION SYSTEMS V/STOL AIRCRAFT CONTROL

    BEELER, E. F. / VOLK, L. J. | SAE Technical Papers | 1965


    Lift fan propulsion systems-V/STOL aircraft control

    Beeler, E.F. / Volk, L.J. | Engineering Index Backfile | 1965