The paper presents real-time non-destructive evaluation (NDE) of fatigue crack damage using ultrasonic sensing. The damage sensing system is suitable for health monitoring and residual life prediction in both aging and new aircraft structures.


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    Title :

    Real-time nondestructive evaluation of airframe structures for health monitoring and residual life prediction


    Contributors:
    Keller, E. (author) / Ray, A. (author)


    Publication date :

    2001-01-01


    Size :

    762904 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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