This paper describes a method which has been developed for estimating the safe fatigue life of compact, highly-stressed and inaccessible components for aeroplanes and helicopters of the Royal Air Force. It is explained why the Design Requirements for British Military Aircraft do not favor the use of a damage-tolerance approach in these circumstances.


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    Title :

    Method of Calculating the Safe Fatigue Life of Compact, Highly-Stressed Components


    Contributors:
    A. W. Cardick (author) / V. J. Pike (author)

    Publication date :

    1994


    Size :

    12 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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