Abstract
The general principles of structural health monitoring by ultrasonic waves with high resolution monitoring of the time dependence of the transport properties are presented. Reported are essential aspects of the theoretical background together with the results of modeling relating to the developed monitoring scheme and the experimental findings. The presented applications of the developed integral structural health monitoring concentrate on examples involving helicopter tails booms. These include conventional aluminum based bolted frame and stringer constructions as well as fiber compound structural components with foam inlays, in both cases for helicopter tail booms. The presentation includes experimental demonstrations on samples suitable for transport.
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