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Numerical Investigation of Structural Health Monitoring of Cracked Metallic Aircraft Structural Panels Repaired with a Bonded FRP Composite Patch

机译:用粘结FRP复合贴片修复裂纹金属飞机结构板结构健康监测的数值研究

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摘要

This paper proposes a method for identifying the shape of a crack in metallic aircraft structural panels repaired with a bonded FRP composite patch by utilizing the measured values of induced in-plane strains in the FRP composite patch under cyclic tensile loading.
机译:本文提出了一种方法,用于通过利用循环拉伸载荷下的FRP复合贴片中的诱导的平面菌株的测量值来识别用粘结的FRP复合贴片修复的金属飞机结构板中的裂缝形状。

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