The simplified formula of ultimate tension load is obtained in view of mix plastic-cone tension failure mode of the M10 plastic embedded part.
针对M 10型预埋件的塑胶-锥体复合拉伸破坏形态，得出极限拉伸荷载的简化计算公式。
In this paper, 9 compressive specimens of 3 groups were tested to investigate the cracking resistant load, ultimate load, failure modes and deformation capacity of the grouted slotted block masonry.
本文通过3组9个抗压试件，了解开槽砌块灌孔砌体的受压开裂荷载、极限承载力、破坏形态和变形能力。
The effect of anchorage schemes on the failure modes and ultimate load capacity of the RC beams strengthened with GFRP sheets are discussed.
分析了梁端锚固形式对玻璃纤维布加固的钢筋混凝土梁破坏形态及极限荷载的影响。
The failure criterion can be judged by the rectangle region in the graph of the relation between ultimate out-of-plane load and ultimate in-plane shear.
它的破坏状态可以用极限面外荷载和极限面面内剪力关系图中围成的矩形区域来判断。
According to the calculated ultimate loads, failure characters, load - deformation curve, and safety coefficients, etc, the bridge is evaluated and some valuable conclusions are attained.
根据分析获得的破坏荷载、破坏特征、荷载位移曲线以及桥梁安全系数等，对该桥设计进行了评价并获得一些有价值的结论。
The ultimate load values, characteristics of failure and load-deflection relationships show good agreement between the finite element and experimental results obtained by other researchers.
由有限元计算所得的极限荷载、破坏特征以及荷载变形关系与试验结果比较接近。
The failure process and mode has been observed, and load-displacement curves, cracking and ultimate load, and the strain of longitudinal and transverse steels have been recorded.
试验中，观测了试件的破坏全过程及破坏形态等，记录了荷载—位移滞回曲线、开裂荷载、极限荷载、箍筋和纵筋的应变等数据。
The ultimate load of cable-stayed bridges is determined by the failure path of structure under the dead load.
在自重荷载作用下，斜拉桥极限承载力与结构的失效路径有关；
Concrete filled in the box shape steel can prevent the early failure of specimens due to the buckling of the box shape steel, and increase the ultimate load.
箱形型钢内浇注混凝土不但可避免型钢屈曲破坏而且还可提高梁的极限荷载。
In this paper the behavior, failure models and ultimate bearing capacity of the two-span continuous wall-beams under the uniformly distributed load is presented.
本文论述了两跨连续墙梁在均布竖向荷载作用下的受力特性、破坏特征和承载能力。
Abstract :Failure process of a primary load-bearing composite joint in wing root was analyzed by finite element methods, and the ultimate strength of the joint was predicted.
以复合材料机翼翼根后梁下缘条对接试件为研究对象，通过有限元手段分析其失效机理和破坏过程，并对极限强度进行预测。
Furthermore, the ultimate load and the failure location of the section vary with the stress-strain relations and initial stress differences of the materials on the section.
承载力和截面破坏控制点因截面上材料的本构关系的变化和应力史差而发生改变。
Furthermore, the ultimate load and the failure location of the section vary with the stress-strain relations and initial stress differences of the materials on the section.
承载力和截面破坏控制点因截面上材料的本构关系的变化和应力史差而发生改变。
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