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首页> 外文期刊>日本機械学会論文集. B編 >Excitation Mechanism of Self--Induced Sloshing Caused by Horizontal Plane Jet
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Excitation Mechanism of Self--Induced Sloshing Caused by Horizontal Plane Jet

机译:水平平面射流引起的自激晃荡的激发机理

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摘要

A self--induced sloshing is excited by flow without any other external force. In a rectangular tank having a horizontal plane jet, the 1 st or 2 nd mode sloshing grow in a certain condition of the inlet velocity and the water level. In this study, the experiment of this phenomenon was conducted and physical characteristics were examined in detail. The new sloshing conditions, i. e. "l st Stage Sloshing" and "2 nd Stage Sloshing", were discovered in a tank. The governing parameter of the sloshing growth, i. e. the modified Strouhal Number St_s, was derived approximately. When St. was nearly either 1.0 (1 st Stage) or 2 .0 (2 nd Stage), the sloshing excitation was arranged consistently. The dependency of the inlet velocity and tank geometry was revealed using St.. A sloshing mode shift or a jet mode (stage) transition was evaluated to give rise to, with varying the inlet jet velocity. Consequently, a feedback mechanism was considered to be validated, which was closed by the jet fluctuation and the sloshing motion. The overall physical oscillation mechanism of the self-induced sloshing was clarified.
机译:在没有任何其他外力的情况下,流动会激发自激晃动。在具有水平平面射流的矩形水箱中,第一或第二模式晃动在入口速度和水位的一定条件下增长。在这项研究中,对该现象进行了实验,并详细检查了其物理特性。新的晃荡条件e。在坦克中发现“第一级晃动”和“第二级晃动”。晃动增长的控制参数,即e。修改后的斯特劳哈尔数St_s近似得出。当St.接近1.0(第1阶段)或2.0(第2阶段)时,晃动激励的布置是一致的。使用St.揭示了进口速度和储罐几何形状的相关性。通过改变进口喷射速度来评估晃动模式的偏移或喷射模式(阶段)的过渡。因此,认为反馈机制已得到验证,该反馈机制因射流波动和晃动而关闭。阐明了自激晃荡的整体物理振荡机理。

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