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Reducing the drag of midpoint lateral orifices of exhaust air ducts by shaping them along vortex zone outlines

机译:通过沿涡旋区域轮廓塑造它们来减少排气管的中点横向孔的拖动

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This study is concerned with the development of an energy-efficient design of a duct fitting comprising a midpoint lateral exhaust orifice. This is an element often encountered in the practice of exhaust ventilation system design and engineering. A numerical study was performed to identify relationships between the drag of such an orifice and its dimensions and the ratio of the airflow entering the orifice and passing through the duct at the confluence, G(O)/G(C). Findings are well supported by other authors' data and by our own experimental study. For the first time, the outlines of a vortex zone occurring at the inlet of the flow have been identified and supported by experimental visualization. A relationship behind orifice dimensions and the flow rate of passing airflow has been determined. A geometric approximation has also been identified for the vortex zone, enabling outlines of any vortex zones to be traced out within the studied range of dimensions and G(O)/G(C) flow ratios. The discovered outlines have been used for an energy-efficient exhaust orifice design featuring reduced drag both for the airflow entering through and bypassing the orifice. A "one-type-fits-all" shape has been identified that minimizes drag over the entire variation range of the G(O)/G(C) ratio. Approximate formulas for all identified relationships have been derived and programmed into an online calculator to facilitate their use in the design of energy-efficient ventilation systems. By making the duct fitting energy-efficient, drag can be reduced by 20-400% compared to a standard design. Reduced pressure losses enable reduction both of power consumption and size/rating of ventilation units used in the system.
机译:本研究涉及开发包括中点横向排气孔的管道配件的节能设计。这是在排气系统设计和工程的实践中经常遇到的元素。进行数值研究以识别这种孔的阻力与其尺寸之间的关系以及进入孔口的气流与通过管道的气流的比率,G(O)/ g(c)。调查结果得到了其他作者的数据和我们自己的实验研究的支持。首次首次,通过实验可视化识别并支持在流入口处发生的涡旋区域的轮廓。已经确定了孔口尺寸背后的关系和通过气流的流速。还识别了涡流区的几何近似,使得任何涡旋区域的轮廓概述才能在研究范围内追踪,G(O)/ g(C)流量比。所发现的轮廓已被用于节能的排气孔设计,其用于进入通过并绕过孔口的气流拖动。已经识别出“单型配合 - 所有”形状,其最小化在G(O)/ g(c)比的整个变化范围内的拖动。所有已识别的关系的近似公式都已推导和编程到在线计算器中,以便于他们在节能通风系统的设计中使用。通过使管道拟合节能,与标准设计相比,拖动可以减少20-400%。减压损失降低能够降低系统中使用的通风单元的功耗和尺寸/额定值。

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