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1)  branch resistance
支盘阻力
1.
It is pointed out that with engineering consideration, the antipulling capacity is dependent on branch resistance.
推导了不同盘间距情况下的支盘桩抗拔承载力的计算公式,并结合工程实例,指出了支盘桩的抗拔承载力主要取决于支盘阻力,为支盘桩的抗拔设计提供了必要的理论依据。
2)  end capacity of disk
支盘端阻力
3)  obstructed round
阻力圆盘
1.
Research on the behavior of obstructed round buoyant vertical jets in static ambient, 2, analysis on the behavior of flow field;
静止环境中有阻力圆盘浮力射流特性的研究——(II)流场特性分析
2.
Research on the behavior of obstructed round buoyant vertical jets in static ambient, 1,verification of mathematical model and numerical method;
静止环境中有阻力圆盘浮力射流特性的研究——(I)数学模型及计算方法的验证
4)  bulb resistance
盘端阻力
1.
The ultimate bearing capacities are determined,the load transfer mechanism is analysed,and the distribution and development of the skin-friction resistances,the bulb resistances and the tip resistances of DX piles of this kind are studied.
通过现场静荷载试验,对以稍密粉砂、中密粉砂和中密粉细砂为承力盘持力层和以中密粉细砂为桩端持力层的四节DX挤扩灌注桩的极限承载力进行判定,分析桩的荷载传递机理,并对桩侧阻力、盘端阻力和桩端阻力的分配及其发展规律进行研究,最后对DX桩在WW大厦的应用情况给予介绍。
2.
Their ultimate bearing capacities is determined,its load transfer mechanism is analysed,and the distribution and development of the skin-friction resistances,the bulb resistances and the tip resistances of DX piles of these two kinds are studied.
通过现场静荷载试验,在膨胀土地基中对桩身穿越大气影响深度并以硬塑黏土为承力盘和桩端持力层的单节DX挤扩灌注桩及以硬塑黏土为上承力盘持力层和以硬塑—坚硬黏土为下承力盘和桩端持力层的两节DX挤扩灌注桩的极限承载力进行判定,分析其荷载传递机理,并对两类桩的侧阻力、盘端阻力和桩端阻力的分配及其发展规律进行研究。
5)  branch force
支盘力
1.
A branch force under some pressure of the hole is obtained based on the data of oil pressure, and then the ultimate bearing capacity of the pile is calculated.
将球形孔扩张理论应用到支盘桩扩孔时径向应力的计算,考虑到扩孔时的油压数据,求得某一孔压下的支盘力,据此估算单桩极限承载力。
6)  support resistance
支架阻力
1.
Research on Failure Laws of Overlying Rock and Support Resistance in Fully-mechanized Face in Shallow Seam of Thick Clay Layers;
厚土层浅埋煤层综采覆岩破坏规律与支架阻力研究
补充资料:肺循环阻力(或全肺阻力)


肺循环阻力(或全肺阻力)
pulmonary circulation resistance

  血液在肺部血管内流动时和血管壁之间的摩擦力和血液内部的摩擦阻力。肺动脉管壁较薄,分支短而管径大,故肺动脉的可扩性较大,对血流的阻力很小,仅0.12PRU(外周阻力单位)。肺循环动脉部分总的阻力和静脉部分总的阻力相等,故血液流动时在动脉部分的压力降落和静脉部分的压力降落相等。
  
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
参考词条