• 本体部分具有相对 相对的

    The body portion has opposing side walls and opposing end walls.

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  • 第一箱体具有相对两个相对的

    The first box is provided with a top wall, two opposite sidewalls and two opposite end walls.

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  • 矩形左边年底是指包括作为实验

    The little rectangle at the left end denotes a small foot end wall: this was included as an experiment.

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  • 在领春木次生木质部观察到了穿孔穿孔板。

    Multiple end wall and lateral-wall perforation plates were also observed in the secondary xylem.

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  • 装焊过程中合缸、对面装配措施独特制造经验

    The measures for shell assembly and end wall face-to-face assembly are special manufacture experience.

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  • 述第二包括,所述端壁包括所述通道连通通孔

    The second end includes an end wall including a hole therein communicating with the passage.

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  • 子机端壁引气能够有效减小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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  • 此外表面向外伸出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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  • 横向流动对角流动分离结构影响大于吸力附面层的分离

    Endwall transverse movement has greater influence on flow separation structure in corner region than separated suction side boundary layer.

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  • 实验结果表明,角区中面层叶面面层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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  • 根据空气预热要求提出冷风预热的方法以及暖风选择原则

    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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  • 一个套筒首先结束第一对套筒第二年底前全部关闭关闭第二端壁

    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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  • 激光多普勒测速系统测量研究了一个离心压气机转子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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  • 详细测量了平行进口端壁附面层设前导两种进口条件下涡轮叶栅出口

    The exit flow fields of a turbine cascade with or without the front guide vanes were investigated.

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  • 针对大折转角子午扩张型导叶通过数值模拟,讨论端壁面层抽吸性能影响

    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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  • 再应用改进了损失激波损失模型最终算出压气机设计点损失沿叶高分布规律

    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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  • 本文介绍平面叶风洞上进行的“孔窝群”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.

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  • 数值模拟清晰地显示了排气缸通道的流场结构是以各种旋涡为主要特征,包括通道分离涡等。

    The computational results revealed a complex vortex system within the casing model, including a passage vortex, a separation vortex and an endwall vortex.

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  • 挡板形成在所述中、在所述通上方,细长装置引入穿过通道通孔时,挡板可运动离开所述第二

    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.

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  • 第二,所述第二端壁通常所述游戏表面垂直伸展并且定位于所述游戏表面与所述第相反的一

    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.

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  • 低速环形叶实验台上圆弧处理轮毂相对静子扩压叶栅环旋转频率对叶栅端壁流动进行了影响实验探索

    An experiment was made in an annual cascade to explore the unsteady flow mechanism of skewed slot hub treatment in removing flow separation near hub.

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  • 发现压气机态特征用于发动机节流过程中工作点接近失速边界的程度的判定,具有一定工程应用价值

    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.

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  • 电化学电池包括一个设有第二、在 第和第二之间延伸以及延伸第一端壁容器

    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.

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  • 实验中不同雷诺数、不同出时通道端壁表面静压分布、压力损失系数、弦向流量分配以及系数进行了测量

    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).

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  • 通过理论分析提出考虑叶片部间隙影响的叶片亏损模型,并对三种压气机边界层叶片力亏损进行了数值计算

    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.

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  • 优化了300MW汽轮机调节采用了子午收缩的弯曲栅,动叶为自带围带销钉三联叶片,再铆接围带形成圈联结叶片。

    The control stage of improved 300MW steam turbine used bowed static blade cascades with convergent tip endwall and integral shroud triple pin rotating blades.

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  • 为了解不同雷诺数流比情况下各种因素压力损失系数影响,对流梯形扰流柱通道端壁静压压力损失系数进行实验测量。

    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.

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  • 为了解不同雷诺数流比情况下各种因素压力损失系数影响,对流梯形扰流柱通道端壁静压压力损失系数进行实验测量。

    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.

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