Review of available statistical data applicable for VTOL operation, and control information obtained during simulated Instrument Flight Rules flight for particular VTOL vehicles with weather conditions simulated at Chance Vought Corp; test results showed that there was not appreciable difference between hovering in still air or hovering at 10 knots under gusty conditions; time histories obtained during still air tests and tests at 30 knots under gusty conditions.


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    Title :

    Gust simulation as applied to VTOL control problems


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1961 VTOL-STOL



    Publication date :

    1961


    Size :

    7 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :