Feasibility study of its use for speed and flight path control during approach phase made with North American Fighter-bomber having J57-P-21A turbojet engine; design development through wind tunnel program selecting and adjusting exhaust gas patterns; flight test program showed that reverser selected produced adequate reverse thrust, up to 40% of net forward thrust, with small effects on aircraft stability, trim, and handling characteristics.


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    Titel :

    Development of in-flight modulating type thrust reverser for single engine aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Kehrer, W.T. (Autor:in)

    Kongress:

    SAE Meeting ; 1960 Thrust reversal



    Erscheinungsdatum :

    1960


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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