AEROSPACE SHANGHAI, Volume. 42, Issue 1, 119(2025)
Multi Damage Self Identification Method for Aerospace Composite Materials Based on Gaussian Clustering
Figures & Tables(8)
Table 1.
Test piece laying condition View tableView in ArticleTable 1.
Test piece laying condition 编号 材料 铺层 1 碳纤维复合材料 [(0/45/-45/90)2 (90/-45/45/0)2] 2 [(45/-45)4 (-45/45)4] 3 [(45/-45)4 (-45/45)4]
Table 2.
Error of damage identification results View tableView in ArticleTable 2.
Error of damage identification results 损伤编号 定位误差/cm 方向角误差/（°） 第1件损伤① 0.04 2.30 第1件损伤② 0.51 2.98 第2件损伤① 0.54 2.52 第2件损伤② 0.09 0.65 第3件损伤① 0.57 2.00 第3件损伤② 0.44 2.48
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Jingya TAO, Yaping YU, Bo LIU, Junming PAN, Guanlin SONG, Zhaoyang WANG, Jian QIAN. Multi Damage Self Identification Method for Aerospace Composite Materials Based on Gaussian Clustering[J]. AEROSPACE SHANGHAI, 2025, 42(1): 119
Paper Information
Category: Integration of Material Structure and Function
Received: Aug. 11, 2024
Accepted: --
Published Online: May. 13, 2025
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