Final Report - AISHA (Aircraft Integrated Structural Health Assessment)
Project ID: 502907Funded under: FP6-AEROSPACE
This is the final report of the AISHA project, which aimed at realising an aircraft monitoring technology by using ultrasonic Lamb waves as the basic sensing principle. The report begins with an introduction on modern structural health methods in aircraft industry and then the project's objectives are described. There is also an analysis of the methodologies explored under the scope of the project and a presentation of the experiments, the full-scale tests and their results, and finally a section about knowledge dissemination actions and use.
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Record Number: 11815 / Last updated on: 2011-04-14