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Transient Response of Nozzels and Diffusors in Pressure-Duct Systems

机译:风管系统中喷嘴和扩散器的瞬态响应

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摘要

This paper attempts to investigate the behavior of pressure waves through nozzels anddiffusors in pressure duct systems. It presents the results of some recent studies in whichthe extent of transmission and reflection of pressure waves of specific throttle types wereinvestigated. In fact there is an unsteady difference between quasi-steady calculationsand the real physical behavior during a pressure wave passage. In order to ascertain theinfluence of a conical throttle (orifice/pipe cross-section area ratio of 1:8) – used once asa nozzle and on the other side as a diffusor - on the transmission of pressure waves, 2arrangements with steel pipe models ( “Straight pipe” and “T-junction”) were conductedin which this throttle element was tested with single pressure waves. For comparison andalso for practical use, the results of the experimental investigations are depicted, afterelimination of additional physical influences, in the form of transmission factors indiagrams. Furthermore, a suitable mathematical approach for computation of thetransmisson behavior is developed. The suitability of application for this unsteadythrottle headloss in the usual unsteady calculation is verified by a standard characteristicmethod (MOC) using control calculations of the experiments. In this unsteady headlossapproach the prehistory of the incident pressure wave is included. Influences of basicflow conditions of the transmission- and reflection behavior are also be described andevaluated.
机译:本文试图研究通过喷嘴和喷嘴的压力波的行为。 压力管道系统中的扩散器。它提出了一些近期研究的结果,其中 特定节流阀类型的压力波的透射和反射程度分别为 调查。实际上,准稳态计算之间存在不稳定的差异 以及压力波通过过程中的实际身体行为。为了确定 锥形节流阀的影响(节流孔/管道截面积比为1:8)–曾经用作 一个喷嘴,另一侧作为扩散器-传输压力波时,2 使用钢管模型(“直管”和“ T型接头”)进行布置 其中该节气门元件已通过单个压力波进行了测试。为了比较和 同样用于实际使用,在下面描述了实验研究的结果 消除其他物理影响,以传播因子的形式 图。此外,还有一种合适的数学方法可用于计算 传输行为得以发展。适用于这种不稳定情况的适用性 通常的非稳态计算中的油门损失通过标准特性进行了验证 方法(MOC)使用实验的控制计算。在这种不稳定的损失中 包括入射压力波的史前过程。基本的影响 还描述了透射和反射行为的流动条件,并且 评估。

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