This report presents the results of the following three research and development activities: the design, fabrication and test of a multi-channel flight control system hybrid simulator; the analysis and application of a flutter damping technique for hydraulically actuated slab type control surfaces; and the experimental testing of Mil-H-83282 hydraulic fluid in a pumping system at elevated temperature.


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    Titel :

    Research and Development of Aircraft Control Actuation Systems. The Development of a Flight Control System Simulator, Research on a Control Surface Flutter Suppression Technique and High Temperature Testing of Mil-H-83282


    Beteiligte:
    G. D. Jenney (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    202 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch