Tác giả CN
| Wagner,H.N.R. |
Nhan đề
| Constant single-buckle imperfection principle to determine a lower bound for the buckling load of unstiffened composite cylinders under axial compression /H.N.R. Wagner ⇑ , C. Hühne, S. Niemann |
Từ khóa tự do
| Buckling |
Từ khóa tự do
| Cylindrical composite shells |
Từ khóa tự do
| Single-perturbation load approach (SPLA) |
Nguồn trích
| Composite structures2016-5
Số: 1
Tập: 139 |
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001 | 16100 |
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002 | 6 |
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004 | 36B44FBD-3965-4381-9FFD-61D5A0D6F4F1 |
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005 | 201708180750 |
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008 | 081223s vm| vie |
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009 | 1 0 |
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039 | |y20170818075644|zcuonglv |
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100 | |aWagner,H.N.R. |
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245 | |aConstant single-buckle imperfection principle to determine a lower bound for the buckling load of unstiffened composite cylinders under axial compression /H.N.R. Wagner ⇑ , C. Hühne, S. Niemann |
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653 | |aBuckling |
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653 | |aCylindrical composite shells |
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653 | |aSingle-perturbation load approach (SPLA) |
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773 | |tComposite structures|v139|i1|d2016-5 |
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890 | |c1|a0|b0|d4 |
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