机译:精确的高阶理论和C〜0有限元用于层合复合材料和夹层板的自由振动分析
Institute for Structural Analysis of Aerocraft, Shenyang Institute of Aeronautical Engineering, Shenyang 110136, China;
Institute for Structural Analysis of Aerocraft, Shenyang Institute of Aeronautical Engineering, Shenyang 110136, China State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, China;
Institute for Structural Analysis of Aerocraft, Shenyang Institute of Aeronautical Engineering, Shenyang 110136, China State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, China;
higher-order theory; C~0 finite element; natural frequency; laminated composite plate; soft-core sandwich plate;
机译:层合复合材料和夹心板的分析和有限元建模:对自由振动响应的新剪切变形理论的评估
机译:热环境下层状复合材料和夹层板振动分析的分段剪切变形理论和有限元公式
机译:使用非多项式之字形模型评估层压复合材料和夹心板的自由振动和弯曲分析:C-0有限元公式。
机译:层压复合板自由振动的有限元分析
机译:叠层复合板的高效高阶理论及有限元实现
机译:软芯和机械性能不均匀的夹层板的自由振动:建模和有限元分析
机译:叠层复合材料和夹层板的自由振动分析:一种层状有限元制剂
机译:夹层复合材料静应力和自由振动分析的有限元技术