Requirements of thrust reverser to reduce aircraft landing runs; examination of four reverser configurations and reasons for discarding them; basic Rolls-Royce reverser design finally adopted is of sleeve valve and clamshell type; design details of outlet vanes, bearings, pneumatic rams and linkage, etc; bench and flight testing. (see also Flight v 75 n 2611 Feb 6 1959 p 187)


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    Titel :

    Thrust reversal for jet aircraft


    Autor / Urheber :

    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print



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