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Evaluation by holographic interferometry of impact damage in composite aeronautical structures

机译:复合航空结构中冲击损伤的全息干涉测量评价

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摘要

The results of an experimental study of holographic interferometry for impact damage detection and evaluation in composite aeronautical sandwich structures is presented. The results show that holographic interferometry using thermal loading can accurately estimate delaminated areas on test samples in respect to ultrasonic inspection. The capability of holographic interferometry for detection of such damages in large composite components is shown also.
机译:介绍了对复合航空夹层结构的冲击损伤检测和评价的全息干涉测量结果的实验​​研究。结果表明,通过热负荷的全息干涉测量法可以精确地估计关于超声波检查的测试样品上的分层区域。还示出了全息干涉测量的能力,用于检测大型复合部件中这种损伤的损伤。

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