The third in a series of three piloted simulations of the Grumman Design 698 Tilt-Fan V/STOL Demonstrator was conducted at NASA Ames Research Center on the Vertical Motion Simulator. Both single-engine-failure characteristics (with and without engine cross-shafting) and hover/low-speed handling qualities were investigated. Based on minimum recovery speed, altitude loss, and ejection capability following a single engine failure, the cross-shafted configuration offers a substantial increase in flight safety over the non-cross-shafted configuration. Based on handling qualities ratings, touchdown performance, and pilot comments, attitude command/attitude hold or translational rate command/translational rate hold response type control systems yield satisfactory handling qualities during shipboard terminal operations.


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    Titel :

    Results of Piloted Simulation of Grumman Design 698


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Johns, John B. (Autor:in) / Clark, John W. (Autor:in) / Donley, Shawn T. (Autor:in)

    Kongress:

    Aerospace Technology Conference and Exposition ; 1985



    Erscheinungsdatum :

    01.10.1985




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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