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inlet flow的中文,翻译,解释,例句

inlet flow

inlet flow的基本解释
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输入流, 吸入流, 输入流量

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Test and analysis show that, the distribution patterns of the tangent veloctiy fields in the big cone area and the small cone area, which are comprised of para-free vortex and para-forced vortex, are basically identical without a change of the radius of the boundary surface; with the increase of the angle of the small cone, the para-free vortex area decreases and the para-forced vortex area increases, and the emulsifiability of the fluid drips increases with the increase of velocity gradient; the tangent velocity increases with the increase of inlet flow, and the maximum tangent velocities of both the big cone area and the small cone area are 4.94 times of the inlet flow; and the maximum tangent velocity increases with the increase of the split ratio and with the radius of the boundary surface not changed.

试验分析表明,大锥段和小锥段切向速度分布规律基本相同,均由准自由涡和准强制涡构成,分界面半径rm没有变化;随着小锥角θ的增加,准自由涡区缩小,准强制涡区扩大,速度梯度增加会加大液滴的乳化程度;随入口流量增加,切向速度增大,经拟合得出大锥段和小锥段的最大切向速度均为入口流量的4.94倍;分流比加大,分界面半径基本不变,最大切向速度增加。

Based on an analysis of distribution pattern of hydrocyclone"s axial velocity, by changing the inlet flow rate Qi and split ratio Fand making an investigation in the effect of Qi and F on axial velocity field, the factors causing the forming of short-cut circuit and circulating flow are found. It is considered that the short-cut circuit and circulating flow are produced by the structure of the hydrocyclone, and can"t be eliminated completely, though they interfere the flow field inside a hydrocyclone and affect the separation accuracy. Test results show that, by increasing Qi and F and controlling them in a certain range, the separation efficiency of the hydrocyclone can be improved.

在研究旋流器轴向速度分布规律的基础上,分析了短路流与循环流的形成原因,试验研究了改变操作参数,即改变入口流量Qi与分流比F对轴向速度场的影响认为短路流与循环流是由旋流器结构决定的,很难完全消除,它们干扰了旋流腔和大锥段的流场,在一定程度上也影响了分离精度试验结果表明,加大入口流量Qi与分流比F,并将其控制在一定范围内,便可提高分离效率这项研究对水力旋流器分离机理的认识与实际应用均有重要意义

Large axial induced draft fan;; inlet box;; internal flow characteristics;; inlet flow conditions;; rectifier object

论文导师吴克启,论文学位硕士,论文专业流体机械及工程论文单位华中科技大学,点击次数 13,论文页数 85页File Size1796K

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two-dimensional flow:二维流动

two-control aircraft 双控飞机 | two-dimensional flow 二维流动 | two-dimensional inlet 二维进气道

compressible flow:可压缩流[动]

对于可压缩流动(compressible flow) ,可定义下面所列的特殊边界条件: 层壁/移动层壁 Wall/moving wall:与不可压缩流动分析相同. 外表流动 External flow:外部流动的外表边界. 超声入口 Supersonic inlet:超声流动内部流动的入口边界.

inlet unstart:进气道熄火

入口溢流 inlet spilled flow | 进气道熄火 inlet unstart | 酸输入口 inlet; acid