- Bài trích
- Nhan đề: Ablation damage assessment of aircraft carbon fiber/epoxy composite and its protection structures suffered from lightning strike /F.S. Wang a, ⇑ , Y.Y. Ji b , X.S. Yu a , H. Chen a , Z.F. Yue a
Tác giả CN
| Wang,F.S. |
Nhan đề
| Ablation damage assessment of aircraft carbon fiber/epoxy composite and its protection structures suffered from lightning strike /F.S. Wang a, ⇑ , Y.Y. Ji b , X.S. Yu a , H. Chen a , Z.F. Yue a |
Từ khóa tự do
| Carbon fiber/epoxy composite |
Từ khóa tự do
| Impulse electrical current test |
Từ khóa tự do
| Lightning strike |
Nguồn trích
| Composite structures2016-6
Số: 1
Tập: 145 |
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001 | 16390 |
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002 | 6 |
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004 | 33920F67-50B7-4C84-912C-E40AF465F86E |
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005 | 201708251518 |
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008 | 081223s vm| vie |
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009 | 1 0 |
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039 | |y20170825152434|zcuonglv |
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100 | |aWang,F.S. |
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245 | |aAblation damage assessment of aircraft carbon fiber/epoxy composite and its protection structures suffered from lightning strike /F.S. Wang a, ⇑ , Y.Y. Ji b , X.S. Yu a , H. Chen a , Z.F. Yue a |
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653 | |aCarbon fiber/epoxy composite |
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653 | |aImpulse electrical current test |
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653 | |aLightning strike |
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773 | |tComposite structures|v145|i1|d2016-6 |
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890 | |c1|a0|b0|d3 |
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