Structural health monitoring of fastener hole using ring-design direct-write piezoelectric ultrasonic transducer
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DOI: 10.1177/14759217211073950
Abstract: Fatigue cracks initiated from fastener holes are common in aircraft structures. Implementation of effective structural health monitoring (SHM) system to detect or monitor fatigue cracks near fastener holes is desired for realizing condition-based maintenance with… read more here.
Keywords: write piezoelectric; crack; direct write; piezoelectric ultrasonic ... See more keywords