Development of Metallic Structure Fatigue Cracks by Composite Patch Repair Using Pre-embedded Fiber Bragg Grating Sensors
碩士 === 國立臺灣大學 === 機械工程學研究所 === 100 === Fatigue is a common failure mechanism in aircraft structures. Composite patching is a recent technique for repairing fatigue cracked structures. However, it is not easy to know whether the crack underlying the composite patch is still growing or not. In this pa...
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| Format: | Others |
| Language: | zh-TW |
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2012
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| Online Access: | http://ndltd.ncl.edu.tw/handle/34493760155426316230 |