(continued from number 2 page 345-363) This paper documents the third phase of a programme of experimental work which validates a structural health monitoring methodology based on novelty detection. In this paper, an extension of the detection method for damage location is proposed and demonstrated. The structure of interest is a Gnat aircraft wing. Although it was not possible to damage the aircraft, the method was demonstrated by determining which of a set of inspection panels had been removed


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    Title :

    Experimental validation of a structural health monitoring methodology: Part 3. Damage location on an aircraft wing


    Additional title:

    Experimentelle Überprüfung einer methode zur Strukturstabilitäts_Überwachung: Teil 3. Schadenslokalisierung an einem Flugzeugflügel


    Contributors:
    Manson, G. (author) / Worden, K. (author) / Allman, D. (author)

    Published in:

    Publication date :

    2003


    Size :

    21 Seiten, 17 Bilder, 8 Tabellen, 11 Quellen




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English