The body portion has opposing side walls and opposing end walls.
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2. 该第一箱体具有一顶壁、两个相对的侧壁和两个相对的端壁。
The first box is provided with a top wall, two opposite sidewalls and two opposite end walls.
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3. 小矩形在左边年底是指一个小足端壁：这是包括作为一个实验。
The little rectangle at the left end denotes a small foot end wall: this was included as an experiment.
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4. 在领春木次生木质部中也观察到了端壁多穿孔板及侧壁穿孔板。
Multiple end wall and lateral-wall perforation plates were also observed in the secondary xylem.
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5. 在装焊过程中合缸、端壁面对面装配等措施是独特的制造经验。
The measures for shell assembly and end wall face-to-face assembly are special manufacture experience.
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6. 所述第二端包括端壁，所述端壁中包括与所述通道连通的通孔。
The second end includes an end wall including a hole therein communicating with the passage.
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7. 静子机匣端壁引气能够有效减小静子叶排损失，提升压气机效率。
Stator casing bleeding can cut the flow loss and improve the compressor efficiency.
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8. 此外，远盖端壁从后表面向外伸出且适合于与相应的远端壁隔开。
Further, the distal cover end wall extends outwardly from the back surface and is adapted to be spaced apart from the corresponding distal end wall.
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9. 端壁横向流动对角区流动分离结构的影响大于吸力面附面层的分离。
Endwall transverse movement has greater influence on flow separation structure in corner region than separated suction side boundary layer.
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10. 韧皮部中筛管分子的端壁是由4—6个梯状排列的筛域组成的复筛板。
The end walls of sieve-tube elements in the phloem have 4-6 specialized sieve areas which together form compound sieve plates.
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11. 该电池还进一步包括具有形成于容器端壁内的厚度缩减槽的卸压排气孔。
The cell further includes a pressure relief vent having a reduced thickness groove formed in the end wall of the container.
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12. 实验结果表明，角区中端壁附面层和叶面附面层的堆积使得叶面附面层变厚；
The result indicated that the interaction between the boundary layer on the suction surface of blade and on the endwall thicken the boundary layer on the suction surface.
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13. 根据空气预热器冷端壁温的要求，提出了冷风预热的方法以及暖风器选择的原则。
Depending upon the requirements of cold end temperature of tube wall of air preheaters, the method of cold air preheating and the criterion of selection for air heater are put forward.
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14. 一个套筒首先结束的第一个端壁和对套筒第二年底前全部关闭是关闭了第二端壁。
A first end of the sleeve is closed by a first end wall and a second end of the sleeve is closed by a second end wall.
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15. 用三维激光多普勒测速系统测量研究了一个离心压气机转子近端壁区三维紊流流场。
Three-dimensional turbulent flow of the endwall region inside a centrifugal compressor impeller was studied using a Laser Doppler Velocimetry.
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16. 详细测量了平行进口端壁附面层与设前导叶两种进口条件下某涡轮叶栅的出口流场。
The exit flow fields of a turbine cascade with or without the front guide vanes were investigated.
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17. 针对某大折转角子午扩张型导叶，通过数值模拟，讨论了端壁附面层抽吸对叶栅性能的影响。
By using of numerical simulation, the effect of applying boundary layer suction on end-wall to the aerodynamic performance for a van with a high-turning Angle and meridional divergence was discussed.
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18. 再应用改进了的端壁损失和激波损失模型，最终算出轴流压气机设计点损失沿叶高的分布规律。
Finally, the total loss distribution along the blade span of the axial flow compressor is estimated according to an improved end wall loss model and a shock loss model.
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19. 本文介绍在平面叶栅风洞上进行的“孔窝群”端壁叶栅和原始(光滑)端壁叶栅对比试验研究结果。
An experimental investigation of end wall flow control for pit-array cascade plate in a compressor cascade wind tunnel has been completed.
The computational results revealed a complex vortex system within the casing model, including a passage vortex, a separation vortex and an endwall vortex.
The flap is formed in the end wall over the hole and is movable away from the second end when an elongate device is introduced through the passage and the hole.
A second endwall extends generally perpendicularly from the playing surface and is located on an opposite side of the playing surface from the first endwall.
The observed end wall flow patterns can be used to assess the stall margins during engine throttling, and thus, it has certain value in engineering application.
The electrochemical cell including a container having a first end, a second end, a side wall extending between the first and second ends, and an end wall extending across the first end.
Experiment measure static pressure, pressure loss coefficient, flow rate of lateral and heat transfer coefficient of endwall at different re and different lateral-flow ratio (c).
A new model is presented for calculating the end-wall boundary layer and its blade force defect inside the axial compressor cascade, based on theoretical analysis.
The control stage of improved 300MW steam turbine used bowed static blade cascades with convergent tip endwall and integral shroud triple pin rotating blades.
The effect of each parameter on distribution of static pressure and pressure loss coefficient are found out. Experiments have been carried out in trapezoidal duct with staggered pin fin arrays.
The effect of each parameter on distribution of static pressure and pressure loss coefficient are found out. Experiments have been carried out in trapezoidal duct with staggered pin fin arrays.
