首页> 外文期刊>Physics of fluids >Flow transients in un-started and started modes of vacuum ejector operation
【24h】

Flow transients in un-started and started modes of vacuum ejector operation

机译:真空喷射器运行的未启动和启动模式中的流动瞬变

获取原文
获取原文并翻译 | 示例
           

摘要

An experimental study has been carried out to investigate the nature of transients in vacuum ejector flows during start-up and the dynamics in flow characteristics. The results show that the secondary stream induction progresses with non-uniform rates with the ramping primary jet pressure during start-up. The initial evacuation period is subjected to gradual and highly perturbed secondary fluid entrainment. In this phase, the secondary stream induction by the shear layer is asymmetric leading to an un-even vacuum generation in the secondary chamber. In the second phase, the secondary pressure fluctuations are found to be ceased for a critical primary jet pressure followed by a rapid induction of the secondary fluid till the primary jet expands to the diffuser wall. The transition from the first phase to the second phase is caused by the secondary stream flow choking in the diffuser. Following the second phase, a stable stage exists in the third phase in which the vacuum pressure decreases only marginally. Any further attempt to increase the secondary chamber vacuum level beyond the third phase, by increasing the primary jet total pressure, results in flow reversal into the secondary chamber, spoiling the already achieved vacuum level. In the fourth phase of start-up, a complicated shock interaction transformation from a Mach reflection (MR) to regular reflection (RR) occurs within the diffuser. It is also observed that the primary jet pressures for the minimum secondary chamber pressure, the minimum secondary pressure, and the primary pressure for MR-RR transformation decrease initially with increase in diffuser length and then increase. It is found that the decreasing and increasing trends are caused by the pressure recovery and Fanno effects, respectively. Published by AIP Publishing.
机译:已经进行了一项实验研究,以研究启动过程中真空喷射器流动的瞬态性质以及流动特性的动态变化。结果表明,在启动过程中,随着初级喷射压力的上升,次级流的诱导以不均匀的速率进行。最初的疏散期要经过逐渐且高度扰动的二次流体夹带。在此阶段,剪切层引起的二次流感应是不对称的,从而导致在二次腔中产生不均匀的真空。在第二阶段中,发现对于临界的一次喷射压力,不再产生二次压力波动,随后迅速引入二次流体,直到一次喷射膨胀至扩散器壁为止。从第一阶段到第二阶段的过渡是由扩散器中的二次流阻塞引起的。在第二阶段之后,在第三阶段中存在一个稳定阶段,在该阶段中真空压力仅略有下降。通过增加一次射流的总压力来进一步增加第二腔室真空度的尝试超出第三阶段,这会导致流反向进入第二腔室,破坏已经达到的真空度。在启动的第四阶段,扩散器内发生了从马赫反射(MR)到正反射(RR)的复杂冲击相互作用转换。还观察到,用于最小次级腔室压力,最小次级压力和用于MR-RR变换的初级压力的初级喷射压力最初随着扩散器长度的增加而减小,然后增加。发现减小和增大趋势分别是由压力恢复和范诺效应引起的。由AIP Publishing发布。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号