This paper defines deflection ratio and designs fair queueing algorithm CFQ basing on dynamic adjustment of weight and having compensation from the method of simulating normalized service of GPS.
本文通过定义偏差率从模拟GPS的规范化服务量角度来设计了基于权值动态调整的具有补偿的公平调度算法CFQ。
Based on meeting the requirements of flexural strength, the effects made by ratio of longitudinal reinforcement on deflection and maximum value of crack width are analyzed.
在满足正截面承载力要求的基础上，分析了纵向配筋率的变化对挠度及最大裂缝宽度的影响。
For this status, this paper proposes a new load ratio deflection method for making monthly trade schedule of directly dispatched thermal power generation units.
针对此现状，提出了一种负荷率偏差法，用于解决直调火力发电单元月度电能交易计划编制问题。
The relationship of deflection, crack spacing and maximum crack width with the stress, diameter and ratio of steel bars can be predicted by existing model presented in the code.
试验梁的挠度、裂缝间距和最大裂缝宽度与钢筋应力、钢筋直径和配筋率等因素的关系基本上可用现有模型预测。
Based on result of lateral actions test, gives load-deflection curves for infilled frames. Influence of aspect ratio on response of infilled frames is analyzed.
通过水平加载的墙板单元试验，得到了墙板单元在水平荷载作用下的荷载—侧移曲线，分析了试件高宽比对墙板单元受力性能的影响。
The equation used to calculate deflection ductility of columns was obtained, which based on the axial compression ratio and hoop characteristic value of a column.
确认分析效果后，对试件进行了计算机模拟的参数分析，得到基于配箍特征值和轴压比的位移延性计算公式。
The effects of the "mass ratio" and "energy ratio" on the deflection at the impinged point are shown by numerical results. The results also indicate that the dynamic plastic deform…
结果表明动态塑性变形主要局限于撞击点附近的区域，因此动态变形模式是与静态塑性破坏机构显著不同的。
The high-aspect-ratio flying wing eliminates vertical tail and conventional rudder, and uses instead a split drag rudder with large deflection as its directional control surface.
大展弦比飞翼布局飞机取消了垂尾和常规方向舵，通常采用大偏角的开裂式方向舵作为偏航操纵面。
The high-aspect-ratio flying wing eliminates vertical tail and conventional rudder, and uses instead a split drag rudder with large deflection as its directional control surface.
大展弦比飞翼布局飞机取消了垂尾和常规方向舵，通常采用大偏角的开裂式方向舵作为偏航操纵面。
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