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   composite material laminate 在 材料科学 分类中 的翻译结果: 查询用时:0.056秒
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  复合材料层板
    ANALYSIS COMPUTATION ON LARGE DEFORMATION OF SMAs COMPOSITE MATERIAL LAMINATE
    SMAs复合材料层板大变形分析计算
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  复合材料层板
    ANALYSIS COMPUTATION ON LARGE DEFORMATION OF SMAs COMPOSITE MATERIAL LAMINATE
    SMAs复合材料层板大变形分析计算
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This paper makes an analysis of the interlaminar shear and tension stresses of the composite material laminate plate by the finite element with three dimensional elements,and a computation of the stress distributions and deformation of the non-symmetric laminate.Analysis is also made of the worping deformation; arising from hygrothermal strain by taking the elastic modulus of the material as a function of temperature and specific moisture concentration

本文用三维体元对复合材料层合板的层间剪切应力和拉(压)应力进行分析,同时计算了非对称层合板的应力分布和变形。文中分析了湿热应变引起的翘曲变形,并考虑了结构材料弹性系数是温度和水分比浓度的函数。

A detailed computation is performed to the vibrating and fluttering characteristic of composite material laminates with different off-axis angles of plies .. A series of data to be used in aeroelastic tailoring purpose is obtained based on the computation, in which the required elastic moduls are provided by fitting the experimental data with the vibration calculated results. Finally, a comparison is demonstrated for three kinds of laminates with different plies compared with corresponding wind tunnel...

A detailed computation is performed to the vibrating and fluttering characteristic of composite material laminates with different off-axis angles of plies .. A series of data to be used in aeroelastic tailoring purpose is obtained based on the computation, in which the required elastic moduls are provided by fitting the experimental data with the vibration calculated results. Finally, a comparison is demonstrated for three kinds of laminates with different plies compared with corresponding wind tunnel test, and a satisfactory agreement is arrived.

本文在一个复合材料层压板上,通过不同的铺设方式和不同的偏轴角,对其振动特性及颤振特性作了详细的计算,得出了一系列有益的、并能说明复合材料层压板可剪裁性的数据。 为了进行上述振动特性的计算,在国内尚没有面外载荷弹性模量的情况下,通过振动试验实测结果,再由振动计算试凑出切实可用的面外载荷弹性模量。 最后,在三种不同铺设的复合材料层压板上作了风洞颤振试验,并取得了与理论计算相一致的结果。

The modulus of SMAs varied with the stage of phase transformation and it brought large recovery stress of restrained recovery. By laying Shape Memory Alloys(SMAs) wires in the composite material laminate,the property of the composite laminate was improved and strengthened. Besides, bending and torsion of the laminate can be found and governed.How to calculate the mechanics behavior correctly is the base of shape control and design and applying of shape memory alloy composite material...

The modulus of SMAs varied with the stage of phase transformation and it brought large recovery stress of restrained recovery. By laying Shape Memory Alloys(SMAs) wires in the composite material laminate,the property of the composite laminate was improved and strengthened. Besides, bending and torsion of the laminate can be found and governed.How to calculate the mechanics behavior correctly is the base of shape control and design and applying of shape memory alloy composite material structures.The nonlinear finite element analysis of the composite laminate includes the thermodynamic behavior and large deformation recovery of the SMAs wires,and by comparing the experimental result with the analytical result, some significant conclusion was obtained.

在复合材料层板结构中铺设形状记忆合金丝 ,利用形状记忆合金弹性模量随相变状态的不同变化 ,受限回复时可以产生很大的回复力的特点 ,除改善和增强复合材料层板本身性能外 ,还能使复合材料层板产生弯曲 ,扭转等形状变化。如何正确有效地计算其力学特性 ,是复合材料层板形状控制以及设计和应用形状记忆合金复合材料智能结构的基础。本文在复合材料层板的有限元分析中考虑形状记忆合金丝的热力学特性以及大变形回复的影响 ,并通过实验进行分析和对比 ,得到一些有意义的结论

 
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