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1)  contact failure
接触失效
1.
Under the action of multiple stresses,contact failure is the main failure mode of aerospace electrical connectors.
在温度和振动等综合应力的作用下,航天电连接器的主要失效形式为接触失效
2)  contact failure prediction
接触失效预测
3)  Tied with failure contact
固连失效接触
4)  jointing loss
接触损失
1.
Subfield Spline finite point method for beams on the elastic ground with jointing loss;
具有接触损失的弹性地基梁的样条子域有限点法
5)  Exposure response
接触-效应
6)  contact effect
接触效应
1.
In this paper, the temperature-dependent thermal and mechanical properties and the contact effect between sub-laminates of delaminated regions on the buckling behavior were considered, and a constrained model was established to ensure deformation compatibility between the sub-laminates al.
采用基于复合材料一阶剪切理论的有限元法研究了含多分层损伤的先进复合材料格栅加筋(AGS)板壳结构的热-机耦合屈曲性态,在屈曲分析中考虑了材料热物理、力学性质与温度相关特性和分层损伤处的上子板、下子板的接触效应。
2.
By using the variational principle of moving boundary and considering the contact effect between delamination regions,the delamination growth was investigated for cylindrical shells under the action of external pressure.
基于可动边界变分原理并考虑脱层间的接触效应对圆柱壳在外部压力作用下的脱层扩展进行了分析,同时应用Griffith准则,导出了脱层前缘各点处的能量释放率表达式,且以轴对称脱层层合圆柱壳为例进行了数值计算,讨论了脱层大小、脱层深度、几何尺寸、材料性质及纤维铺层方式等因素对脱层扩展的影响。
3.
Considering the variational principle of moving boundary and the contact effect between delamination regions, the nonlinear governing equations for delaminated beams subjected to transverse linear load are derived, and the corresponding boundary and matching conditions are given.
基于可动边界变分原理对层合梁脱层扩展进行了分析;考虑了脱层间的接触效应,建立了层合梁在横向线载荷作用下的非线性控制微分方程及相应的定解条件;应用Griffith准则导出了脱层前缘各点处的能量释放率表达式;通过算例讨论了脱层长度、脱层深度、几何尺寸、材料性质等因素对脱层扩展的影响。
补充资料:发育进度预测法(见发生期预测)


发育进度预测法(见发生期预测)


  发育进度预测法见发生期预测。
  
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