Integrated and flexible ultrasonic transducers for structural health monitoring on aircraft structures
Fatigue crack initiating from fastener holes in aluminum plates is a typical damagefrequently found on modern aircraft structures. Requirements for life extension of agingaircraft fleets and reduced maintenance costs have been accelerating the developments ofstructural health monitoring (SHM) techno...
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| Format: | Others |
| Language: | en |
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McGill University
2010
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| Online Access: | http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=97155 |