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 Roy Aeronautical Soc -- J v 63 n 586 Oct 1959 p 563-71)


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    Title :

    Thrust reversal for jet aircraft


    Additional title:

    Flight


    Contributors:

    Published in:

    Flight ; 75 , n 2611


    Publication date :

    1959


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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