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首页> 外文期刊>Journal of Fluid Mechanics >Starting flow through nozzles with temporally variable exit diameter
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Starting flow through nozzles with temporally variable exit diameter

机译:通过流出口直径随时间变化的喷嘴开始流动

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Starting flow through a nozzle or orifice typically results in the transient formation of a leading vortex ring and trailing jet. Experiments are conducted to investigate the dynamics of this process in the case of a temporally variable nozzle exit diameter, with the aim of understanding these flows as they occur in Nature and emerging technologies. By kinematically decoupling the source flow from the nozzle motion, comparison across several classes of exit diameter temporal variation is facilitated. Kinematic models of the starting flows are used to accurately predict the fluid circulation produced by the vortex generators, and to emphasize the special role of the nozzle boundary layer in dictating the nature of the global flow patterns. A dimensionless temporal parameter is derived in order to track the vortex formation process for the various classes of nozzle motion. Dynamics of vortex ring disconnection from the source flow are studied in this new dimensionless framework. We show that temporally increasing the nozzle exit diameter as the starting flow develops results in higher-energy vortex ring structures with peak vorticity located further from the axis of symmetry relative to a static nozzle case. In addition, the normalized energy supplied by the vortex generator is increased in this process. We do not observe a delay in the onset of vortex ring disconnection from the trailing jet, as predicted by previous numerical simulations. In contrast, growth of the leading vortex ring is substantially augmented by temporally decreasing the nozzle exit diameter during fluid ejection, as noted in a previous experiment. Normalized vortex ring circulation is increased 35% in these cases, and the normalized energy of the generated vortex rings is equivalent to that of Hill's spherical vortex. These observed effects are explained by considering the measured vorticity distribution and energy of the starting flows. Strategies are suggested to exploit the discovered dynamics for various pulsed-jet applications.
机译:通过喷嘴或孔口的起始流通常会导致前涡流环和尾流的过渡形成。进行实验以调查在喷嘴出口直径随时间变化的情况下该过程的动力学,目的是了解这些流动在自然界和新兴技术中的发生。通过运动方式将源流从喷嘴运动中解耦出来,可以简化几种出口直径随时间变化的比较。起始流动的运动学模型可用于准确预测涡流发生器产生的流体循环,并强调喷嘴边界层在决定总体流动方式的性质方面的特殊作用。导出无量纲的时间参数,以便跟踪各种类型的喷嘴运动的涡流形成过程。在这个新的无量纲框架中研究了涡流环与源流的分离动力学。我们显示,随着起始流量的发展,临时增加喷嘴出口直径会导致高能涡流环结构,其峰值涡度相对于静态喷嘴情况更远离对称轴。另外,在该过程中,由涡流发生器提供的归一化能量增加。正如先前的数值模拟所预测的,我们没有观察到涡流环从尾随喷射流中断开的延迟。相反,如先前实验中所指出的,通过在流体喷射过程中暂时减小喷嘴出口直径来显着增强前涡流环的生长。在这些情况下,归一化涡旋环的循环增加了35%,并且所生成涡旋环的归一化能量等于希尔的球形涡旋的能量。这些观察到的影响通过考虑测得的涡流分布和起始流的能量来解释。建议采取各种策略,以将发现的动力学用于各种脉冲喷射应用。

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