Thrust reverser proved to be very reliable turbojet accessory which operated successfully and economically for over 4 yr; it has merit of being aircraft carried braking system which is retractable and has small associated performance loss if properly installed; installation features which affect available reversed thrust; ingestion of gas or stones may severely limit thrust reverser effectiveness and prove expensive to airline operator in engine repairs if it is not dealt with during power plant design; method of simulating problem at model scale was established and confirmed by full scale results on several transports powered by Rolls Royce engines.


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    Title :

    Thrust reverser performance and ingestion problem


    Additional title:

    AGARD -- Report


    Contributors:
    Brown, D.M. (author)

    Published in:

    Publication date :

    1963


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




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