Damage Location and Assessment of Composite Material Structure Based on Optical Fiber Sensor Network
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Abstract
A method for damage positioning and assessing the aircraft composite material structure by burying the orthogonal plastic optical fiber sensor network into the structure was proposed. The results show that by this method, problems like whether the composite structure was damaged or where the damage location was, could be quickly and accurately determined, so the damage location and assessment of composite material structure were achieved on line.
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