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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    Title :

    Thrust reversal for jet aircraft


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1959


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Thrust reversal for jet aircraft

    Colley, R.H. | Engineering Index Backfile | 1959


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