Eddy current analysis of mid-bore and co
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P.R. Underhill; T.W. Krause
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Article
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2011
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Elsevier Science
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English
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Fatigue cracks are prone to develop around fasteners found in multi-layer aluminum structures on aging aircraft. Probability of Detection (POD) studies using eddy current techniques within the bolt holes contribute to risk assessments used in evaluating the serviceability of these aircraft. The sign