Stability of laminated composites with delaminations
In this thesis, investigation on buckling problem of composite beam is carried out. A new formula which is denoted as CLT method 3 is derived to calculate the effective flexural stiffness of the thin composite beam. Two other existing equations indicated as CLT methods 1 and 2 that can also be used...
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| 格式: | Thesis |
| 语言: | English |
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2010
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| 在线阅读: | https://hdl.handle.net/10356/39704 |