摘要: Dynamic instability of a laminated composite panel subjected to a transverse load is studied. Up to cubic variations in the thickness coordinate are included in the inplane displacement field, and only the constant component is ke... 展开
作者 | Taylor, W. W. | ||
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原报告号 | ADA230610 | 总页数 | 98 |
主办者 | Non Paid ADAS | ||
报告分类号 | [71F - Composite Materials, 41K - Engineering Materials] | ||
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Composite structures Laminates Collapse Coordinates Displacement Dynamic response Dynamics Finite element analysis Graphs Integration Numerical analysis Panels Quadratic equations Shear properties Stability Static loads Strain(Mechanics) Thickness Transverse Laminated composite panels Shells(Structural forms) Nonliner analysis Vibration Structural mechanics Dynamic instability Theses Loads(Forces) |