The current status of flight simulation fatigue crack growth concepts is reviewed. Crack growth models and methods of crack growth prediction are compared with respect to applicability and limitations. Research areas for improvement of crack growth prediction are specified.


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    Title :

    Current Status of Flight Simulation Fatigue Crack Growth Concepts


    Contributors:

    Publication date :

    1988


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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