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Geometrically Nonlinear Random Responses of Stiffened Plates Under Acoustic Pressure 被引量:1
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作者 YANG Shaochong LI Youchen +1 位作者 YANG Qingsheng WANG Jianmin 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2020年第5期726-738,共13页
An algorithm integrating reduced order model(ROM),equivalent linearization(EL),and finite element method(FEM)is proposed to carry out geometrically nonlinear random vibration analysis of stiffened plates under acousti... An algorithm integrating reduced order model(ROM),equivalent linearization(EL),and finite element method(FEM)is proposed to carry out geometrically nonlinear random vibration analysis of stiffened plates under acoustic pressure loading.Based on large deflection finite element formulation,the nonlinear equations of motion of stiffened plates are obtained.To reduce the computation,a reduced order model of the structures is established.Then the EL technique is incorporated into FE software NASTRAN by the direct matrix abstraction program(DMAP).For the stiffened plates,a finite element model of beam and plate assembly is established,in which the nodes of beam elements are shared with shell elements,and the offset and section properties of the beam are set.The presented method can capture the root-mean-square(RMS) of the stress responses of shell and beam elements of stiffened plates,and analyze the stress distribution of the stiffened surface and the unstiffened surface,respectively.Finally,the statistical dynamic response results obtained by linear and EL methods are compared.It is shown that the proposed method can be used to analyze the geometrically nonlinear random responses of stiffened plates.The geometric nonlinearity plays an important role in the vibration response of stiffened plates,particularly at high acoustic pressure loading. 展开更多
关键词 stiffened plate acoustic loading geometric nonlinearity random vibration equivalent linearization
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含分层损伤复合材料层合结构在弯曲载荷作用下的屈曲问题研究 被引量:8
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作者 陈金龙 宫文然 李峰 《中国科学:技术科学》 EI CSCD 北大核心 2015年第5期464-470,共7页
由于制造缺陷和服役过程中的外物冲击,分层损伤是广泛存在于复合材料层合结构中的一种缺陷形式.本文研究含圆形分层损伤碳纤维增强型层合结构在四点弯曲载荷作用下的屈曲力学行为.用三维数字图像相关技术获取屈曲表面的变形场和应变场,... 由于制造缺陷和服役过程中的外物冲击,分层损伤是广泛存在于复合材料层合结构中的一种缺陷形式.本文研究含圆形分层损伤碳纤维增强型层合结构在四点弯曲载荷作用下的屈曲力学行为.用三维数字图像相关技术获取屈曲表面的变形场和应变场,并以3自由度的利兹法为基础建立反映含分层损伤层合结构在弯曲载荷作用下屈曲力学行为的一维理论模型.最后,用实验得出的屈曲临界载荷值验证理论模型计算出的屈曲临界载荷值,并得出结论:本文提出的计算分层屈曲临界载荷的简便方法,可以用于屈曲临界载荷的初步估算. 展开更多
关键词 分层损伤 碳纤维增强层合结构 屈曲行为 三维数字图像相关 四点弯曲
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