Abstract
Critical aircraft structures are susceptible to hidden corrosion. Find-it and fix-it approaches are inefficient as it relates to managing the problems associated with corrosion. More comprehensive corrosion information may be obtained using data fusion from several detection and evaluation methods. To this end, microwave, conventional and pulsed eddy current data from a multi-layer corroded panel, representing an aircraft lap joint, are fused and used as inputs to a structural analysis model to obtain a comprehensive snapshot of the corroded environment. This paper presents the data fusion algorithm and the structural analysis model along with a discussion of the results.
| Original language | English |
|---|---|
| Title of host publication | Review of Progress in Quantitative Nondestructive Evaluation: Portland, Oregon, 30 July-4 August 2006 |
| Publisher | American Institute of Physics |
| Pages | 611-618 |
| Number of pages | 8 |
| ISBN (Print) | 9780735403994 |
| Publication status | Published - 2007 |
| Event | Symposium on Quantitative Nondestructive Evaluation - Duration: 30 Jul 2006 → … |
Conference
| Conference | Symposium on Quantitative Nondestructive Evaluation |
|---|---|
| Period | 30/07/06 → … |
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