2004
DOI: 10.1007/978-3-662-08988-0_1
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Degradation of Aircraft Structures

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Cited by 4 publications
(2 citation statements)
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“…But conventional NDT can only detect macroscopic cracks, after about 90% of the fatigue life has been consumed. 1) Therefore, early detection of fatigue damage has been required in respect to their maintenance and safety management. In order to detect fatigue damage at an early stage, it is necessary to detect changes in the dislocation structure, microcracks, and closed cracks associated with fatigue damage, which is however very difficult with general UT using linear ultrasonic waves.…”
Section: Introductionmentioning
confidence: 99%
“…But conventional NDT can only detect macroscopic cracks, after about 90% of the fatigue life has been consumed. 1) Therefore, early detection of fatigue damage has been required in respect to their maintenance and safety management. In order to detect fatigue damage at an early stage, it is necessary to detect changes in the dislocation structure, microcracks, and closed cracks associated with fatigue damage, which is however very difficult with general UT using linear ultrasonic waves.…”
Section: Introductionmentioning
confidence: 99%
“…Numerous NDT techniques were used for the assessment of impact damage in composite laminates. 10 Impact-induced delamination in such materials was imaged by digital shearography, 11 which demands sensitive and expensive instruments as well as highly skilled inspectors for the use of this technique. In addition, the lack of clarity of defects deep beneath the surface also limits the application.…”
Section: Introductionmentioning
confidence: 99%