Identification of Location and Shape of Fatigue Crack Fronts in Aircraft Structural Panels Repaired with a Bonded FRP Composite Patch Containing a Strain Measurement Plane
Identification of Location and Shape of Fatigue Crack Fronts in Aircraft Structural Panels Repaired with a Bonded FRP Composite Patch Containing a Strain Measurement Plane
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识别用含有应变测量平面的粘合 FRP 复合材料补片修复的飞机结构面板中疲劳裂纹前沿的位置和形状
DOI：
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发表时间：
2004
期刊：
影响因子：
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通讯作者：
S.Fujimoto
中科院分区：
文献类型：
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作者：
S.Fujimoto
