EXPERIMENTAL VALIDATION OF A STRUCTURAL HEALTH MONITORING METHODOLOGY: PART III. DAMAGE LOCATION ON AN AIRCRAFT WING |
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| Authors: | G MANSON D ALLMAN |
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| Institution: | a Dynamics Research Group, Department of Mechanical Engineering, University of Sheffield, Mappin Street, Sheffield, S1 3JD, Englandf1k.worden@sheffield.ac.ukf1b Aero-Structures Department, Mechanical Sciences Sector, Glauert Building (A9), DERA ††Now QinetiQ., Farnborough, Hampshire, GU14 0LX, England |
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| Abstract: | 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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