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Measurement Of Pressure Profile Of Vortex Flashing Flows In Convergent-Divergent Nozzles

机译:涡旋闪光流动压力曲线在收敛 - 发散喷嘴中的测量

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Vortex control is a novel two-phase convergent-divergent nozzle restrictiveness control mechanism which requires no change to the physical dimensions of the nozzle geometry. The control is achieved by adjustable nozzle inlet vortex. This novel control mechanism can potentially provide flow control with less sacrifice of nozzle efficiency, which is extremely important for ejector cooling cycle performance. It is also less vulnerable to clogging since the flow control is achieved without changing the flow area. However, the underlying mechanism behind the vortex control is still unclear. Measurement of the pressure profile of the vortex flashing flows in convergent-divergent nozzles under different conditions can provide more insights into the vortex nozzle flows and help to explain the vortex control mechanism. It also provides validation for modeling of vortex flashing flows. In this study, the experimental investigation of the pressure profile of the vortex flashing flows is presented. For initially subcooled conditions the pressure drop in the divergent part of the nozzle has been increased due to the vortex. This is mainly due to the more vapor generation in the divergent part caused by the applied vortex. Since the fluid is single-phase liquid in the convergent part of the nozzle, with elevated pressure at the throat and constant inlet conditions, the nozzle mass flow rate is therefore reduced. Vapor quality at different axial locations relative to the nozzle throat has been estimated with a proposed 1D model for initially subcooled conditions based on the measured pressure profile and mass flow rates. It has been shown that the applied vortex makes the outflow much closer to thermodynamic equilibrium than without vortex. By the introduction of inlet vortex, the isentropic efficiency of the nozzle has been improved from 29% to 55%.
机译:涡旋控制是一种新型的两相会聚 - 发散喷嘴限制性控制机构,其不需要改变喷嘴几何形状的物理尺寸。通过可调节的喷嘴入口涡流来实现控制。这种新颖的控制机构可以通过更小的喷嘴效率提供流量控制,这对于喷射器冷却循环性能非常重要。由于在不改变流量面积的情况下实现了流量控制,因此它也易受堵塞。然而,涡旋控制背后的潜在机制仍然不清楚。在不同条件下会聚 - 发散喷嘴中涡旋闪光流的压力曲线的测量可以为涡流喷嘴流提供更多的见解,并有助于解释涡流控制机制。它还提供涡流闪烁流的建模验证。在该研究中,提出了涡旋闪光流的压力分布的实验研究。对于初始过冷条件,由于涡流,喷嘴的发散部分中的压降已经增加。这主要是由于施加的涡旋引起的发散部分中的蒸气产生越多。由于流体是喷嘴的会聚部分中的单相液体,因此在喉部处具有升高的压力和恒定入口条件,因此减少了喷嘴质量流量。在基于测量的压力分布和质量流量的基础上,已经用初始过冷条件的提出的1D模型估计了相对于喷嘴喉部的不同轴向位置处的蒸汽质量。已经表明,所施加的漩涡使流出更接近热力学平衡而不是没有涡流。通过引入入口涡流,喷嘴的等熵效率从29%提高到55%。

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