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The significance of vortex ring formation to the impulse and thrust of a starting jet

机译:涡流环形成对初始射流的冲量和推力的重要性

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The recent work of Gharib, Rambod, and Shariff [J. Fluid Mech. 360, 121 (1998)] studied vortex rings formed by starting jets generated using a piston-cylinder mechanism. Their results showed that vortex rings generated from starting jets stop forming and pinch off from the generating jet for sufficiently large values of the piston stroke to diameter ratio (L/D), suggesting a maximization principle may exist for propulsion utilizing starting jets. The importance of vortex ring formation and pinch off to propulsion, however, rests on the relative contribution of the leading vortex ring and the trailing jet (which appears after pinch off) to the impulse supplied to the flow. To resolve the relative importance of the vortex ring and trailing jet for propulsion, a piston-cylinder mechanism attached to a force balance is used to investigate the impulse and thrust generated by starting jets for L/D ratios in the range 2-8. Two different velocity programs are used, providing two different L/D values beyond which pinch off is observed, in order to determine the effect of vortex ring pinch off. Measurements of the impulse associated with vortex ring formation show it to be much larger than that expected from the jet velocity alone and proportionally larger than that associated with a trailing jet for L/D large enough to observe pinch off. The latter result leads to a local maximum in the average thrust during a pulse near L/D values associated with vortex rings whose circulation has been maximized. These results are shown to be related to the nozzle exit over-pressure generated during vortex ring formation. The over-pressure is in turn shown to be associated with the acceleration of ambient fluid by vortex ring formation in the form of added and entrained mass. (C) 2003 American Institute of Physics. [References: 25]
机译:加里卜,兰博德和沙里夫[J.流体机械。 [H.Med.Chem.Soc。,360,121(1998)]研究了通过使用活塞-气缸机构产生的喷射流形成的涡环。他们的结果表明,对于足够大的活塞冲程直径比(L / D),启动射流产生的涡流环停止形成并从生成射流中挤压,这表明利用启动射流进行推进可能存在最大化原理。然而,形成涡流环并夹住推进力的重要性在于前导涡流环和尾随射流(夹断后出现)对提供给流动的冲动的相对贡献。为了解决涡流环和尾随射流对推进的相对重要性,使用了一个与力平衡装置相连的活塞-气缸机构,以研究在2-8范围内的L / D比率下,由起动射流产生的脉冲和推力。使用两个不同的速度程序,提供两个不同的L / D值,超过该值可以观察到夹断现象,以便确定涡流环夹断的效果。与涡流环形成相关的冲动的测量结果表明,它比单独从射流速度所预期的要大得多,并且与L / D的尾随射流所产生的冲动成比例地大,足以观察夹断。后者的结果导致在脉冲附近的L / D值接近其循环已最大化的涡流环的平均推力的局部最大值。这些结果表明与涡流环形成过程中产生的喷嘴出口过压有关。反过来,该超压显示为通过以附加和夹带质量的形式形成涡流环而与环境流体的加速相关联。 (C)2003美国物理研究所。 [参考:25]

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