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Experimental investigation of ventilated supercavitation under unsteady conditions

机译:不稳定条件下通风超渗流的实验研究

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Ventilated supercavitation is a promising technique to achieve high-speed transport underwater by generating a gas bubble enclosing a moving object through ventilation. However, implementing this technique requires clear understanding and precise control of supercavity behaviors under unsteady conditions in practical applications. In this study, we present the systematic investigation of ventilated supercavity behaviors over a broad range of unsteady conditions. The experiments are conducted in the high-speed water tunnel at Saint Anthony Falls Laboratory. The unsteady conditions are generated using a gust generator consisting of two flapping hydrofoils mounted upstream of a forward-facing cavitator. We use high-speed imaging to capture the variation of cavity dimension and flow patterns along with simultaneous pressure measurements. Measurements are conducted under fixed tunnel speed and ventilation rate with the flapping hydrofoils operating under varying angle of attack (AoA) and frequency (f_g). The visualization and pressure signals reveal five distinct states of supercavity under unsteady conditions, referred to as stable state, wavy state, pulsating state Ⅰ, pulsating state Ⅱ and collapsing state. The stable state occurs under low AoA and f_g, the supercavity only exhibits small amplitude of oscillation without appreciable deformation of the cavity interface. When the supercavity is at wavy state (moderate AoA and high f_g), the supercavity displays clear periodic wavelike deformation of its surface with cavity pressure varies periodically at two times of f_g Under high AoA with low f_g, pulsating state 1 of the cavity shows significant fluctuations in length with intermittent shed-off of gas pockets at the rear part of the cavity. With increase of f_g, the cavity exhibits enhanced pulsating behavior and a sharp of difference between cavity pressure and test section pressure (i.e. pulsating state Ⅱ). At the highest AoA (i.e. AoA 10°) and/j above 2 Hz, the cavity collapses. The transition across different supercavity states under a broad range of unsteady conditions is summarized in the supercavity state map, showing the dependence of supercavity states on the characteristic scales of unsteadiness in comparison to longitudinal and lateral dimensions of the supercavity.
机译:通风的超级空间是一种有希望的技术,通过通过通风产生围绕移动物体的气泡来实现水下的高速运输。然而,实施该技术需要在实际应用中的不稳定条件下清楚地了解并精确控制超级条件。在这项研究中,我们在广泛的不稳定条件下提供了对通风超级行为的系统调查。实验在圣安东尼瀑布实验室的高速水隧道中进行。使用由安装在前部空腔上游的两个凸起的水翼组成的燃气发生器产生不稳定的条件。我们使用高速成像来捕获腔尺寸和流动模式的变化以及同时压力测量。测量在固定的隧道速度和通风速率下进行,与在不同的攻角(AOA)和频率(F_G)下操作的扑振水翼。可视化和压力信号在不稳定条件下显示五个不同的超级障碍状态,称为稳定状态,波浪状态,脉动状态Ⅰ,脉动状态Ⅱ和折叠状态。在低AOA和F_g下发生稳定状态,超级避难度仅表现出小的振荡幅度,而不会明显变形腔界面。当超级沟率处于波状状态时(中等AOA和高f_g),超级避险度显示其表面的清晰周期性波动变形,其表面具有腔压在高AOA下的两次与低f_g下的两个次数周期性,腔的脉动状态1显示出显着在腔后部的气袋间歇性脱落的长度的波动。随着F_G的增加,腔具有增强的脉动行为和腔压和试验段压力之间的差异突出(即脉动状态Ⅱ)。在最高的AOA(即aoA 10°)和/ J以上2 Hz,腔塌陷。在超级沟率状态图中总结了不同超级条件下不同超级沟壑状态的过渡,示出了超级沟壑状态对超级避险度的纵向和横向尺寸相比,超宽度状态对不稳定性的特征尺度的依赖性。

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