A small pump with an extended suction duct that is designed to pump fluid from barrels.
一种带延伸的吸入导管的小泵，用来从桶中泵出流体。
The results suggest that the effects of buoyancy force, variable physical properties of the fluid, and duct geometric characteristic on flow and heat transfer can be very significant.
研究表明，流体剧烈变化的热物性、浮升力以及三角管的几何特征对管内流动换热的影响非常明显。
Conclusion: the components in rete testis fluid can regulate the EGFR expression and structure of epididymal duct in initial segment and corpus through different mechanism.
结论：睾丸网液的成分通过不同作用机制影响附睾起始部和体部的结构和EGFR的表达。
The heat transfer and characteristics of the fluid flow in the duct of the trailing edge of the turbine blade with parted pin-fin arrays were experimentally investigated.
本文对具有断裂结构扰流柱的涡轮叶片尾缘楔型通道的流动与换热过程进行了实验研究。
Conclusion the operation can disengage pancreatic duct obstruction, drain away the pancreatic fluid, prevent reflux and anastomotic leakage, is an effective treatment for pancreatic lithiasis.
结论术式能彻底解除胰管梗阻，引流胰液，有效地抗返流及预防吻合口瘘，不失为治疗胰管多发性结解除梗阻石的有效方法。
Meanwhile, a group of experimental data of additional noise pressure level and fluid pressure loss generated by flow in a duct is presented to explain the readability of us...
由于声激波降噪需要附加一段具有高速流动的缩放管道，它会附加流动噪声和压力损失，本文提供了这方面的一组实验数据，以说明应用声激波消声器的现实可能性。
The computational fluid dynamics (CFD) analysis of air-flow generating duct were utilized for sampling scheme given by uniform design to collect the train dataset.
利用均匀设计安排试验方案，并通过流体动力学仿真完成训练样本采集。选定相关向量机作为优化设计的评估函数。
An experimental study has been carried out for the forced convection heat transfer in non-Newtonian fluid in a small scale square duct at low Reynolds Numbers.
对非牛顿流体在小尺寸方形通道内的低雷诺数受迫对流传热进行了实验研究。
Conclusion the operation can disengage pancreatic duct obstruction, drain away the pancreatic fluid, prevent reflux and anastomotic leakage, is an effect...
结论术式能彻底解除胰管梗阻，引流胰液，有效地抗返流及预防吻合口瘘，不失为治疗胰管多发性结解除梗阻石的有效方法。
The heat transfer and characteristics of the fluid flow in the duct with waist-shaped pin - fin arrays for the trailing edge of the turbine blade were experimentally investigated.
本文对涡轮叶片尾缘中具有束腰结构扰流柱的冷却通道的传热和流动阻力特性进行了实验研究，重点研究了雷诺数、扰流柱的束腰比以及不同组合的影响。
The dual magnet circuit is designed with the magnets. The magnetic induced intensity in the duct is raised to 0 78T. The principle experiment is performed by the jetting fluid of the rocket engine.
设计了双磁回路，通道内磁感应强度提高到0．78T，用火箭发动机的射流作为工作源，进行了发电原理实验；
The dual magnet circuit is designed with the magnets. The magnetic induced intensity in the duct is raised to 0 78T. The principle experiment is performed by the jetting fluid of the rocket engine.
设计了双磁回路，通道内磁感应强度提高到0．78T，用火箭发动机的射流作为工作源，进行了发电原理实验；
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