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弯矩作用下火箭对接面螺栓拉力分布规律探讨 被引量:5
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作者 袁彪 王淑范 敖林 《导弹与航天运载技术》 北大核心 2003年第2期37-40,共4页
对火箭结构总体设计中弯矩作用下壳段对接螺栓拉力计算方法进行了分析 ,指出其中的不合理性 ,并采用有限元法对壳段典型对接形式进行了数值计算 ,探讨了对接端框厚度、螺栓分布圆半径及螺栓数目对螺栓拉力。
关键词 火箭结构 总体设计 弯矩作用 对接面 螺栓 拉力分布规律
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Stretch rate and deformation for pre-stretching aluminum alloy sheet 被引量:2
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作者 朱才朝 罗家元 《Journal of Central South University》 SCIE EI CAS 2012年第4期875-881,共7页
Numerical simulation combined with experimental test was carried out to analyze the pre-stretching process of the 7075 aluminum alloy sheet,from which the stress variation curves and residual stress of aluminum alloy ... Numerical simulation combined with experimental test was carried out to analyze the pre-stretching process of the 7075 aluminum alloy sheet,from which the stress variation curves and residual stress of aluminum alloy sheet in different stretch rates were obtained.The results show that the residual stress in length direction is released after unloading the stretch force,while the residual stress in width direction is released during the stretching process.The study of residual stress elimination is beneficial for optimizing stretch rate on the basis of residual stress distribution law.By comparing the variation principle of residual stress in length direction,the size range of three deformation areas and elimination percentage of residual stress were obtained.The residual stresses of clamping area and transition area are not eliminated effectively,so sawing quantity should be the sum of both the areas.The elimination rate of residual stress in even deformation area could reach 90% after choosing a proper stretch rate,which is verified by both simulation and experiment. 展开更多
关键词 residual stress stretch rate defonnation area sawing quantity
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