... all-plastic molded全塑模注的 warping stress翘曲应力 fuselage fairing机身整流装配 ...
基于628个网页-相关网页
The sunlight temperature load and the abruptly temperature reduction load and the annual temperature load are put forward at the first. It is point out that these temperature loading can beget telescopic stress and warp stress in slab.
提出温度荷载的类型主要有日照温度荷载、骤然降温荷载和年温度荷载，并指出温度荷载将使轨道板受到伸缩应力和翘曲应力。
参考来源 - 板式无砟轨道温度力研究·2,447,543篇论文数据，部分数据来源于NoteExpress
建立有限元模型，计算配置两种材料道面的荷载应力与翘曲应力并进行比较。
By setting up finite element model, the load stress and the warping stress of the two materials pavement are calculated and compared.
为使剪滞翘曲应力满足轴向自平衡条件，选取了新的翼缘板纵向翘曲位移模式。
A new warping displacement mode of wide flange is chosen to meet the axial self-equilibrium condition for corresponding stress.
道面板的尺寸是由飞机荷载和温度(包括伸缩应力和翘曲应力)共同作用所决定的。
Based on analyzing the loading stress and the temperature stress (including contraction stress and warping stress), a calculating method of the slab size is set up.
应用推荐