UNTIL about ten years ago the basis for the design of aircraft landing gear was an arbitrary set of static strength requirements as specified in the British Civil Airworthiness Requirements or Av.P.970, which experience had shown provided an acceptable standard of safety. The number of landings achieved by most military aircraft, however, seldom exceeded one or two thousand and the fatigue performance was, therefore, generally acceptable.


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    Title :

    Some Fatigue Problems Encountered in the Design of an Aircraft Landing Gear


    Subtitle :

    An account of the methods used to ensure adequate fatigue life in undercarriage design


    Contributors:


    Publication date :

    1968-01-01


    Size :

    13 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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