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文章针对均匀流场中三维深型陷落腔因流分离而产生的流激振荡问题开展了一系列的实验研究.在来流流速为0攻角时实验时的雷诺数变化范围:Re=1.55×105~8.74×105.实验中分别测量了三维深型陷落腔侧壁周向及垂向流体压力,分析了腔体内脉动压力周向、垂向的分布规律及腔口处剪切层自持振荡特性.实验结果表明:均匀流场中三维深型陷落腔内脉动压力分布较为复杂.在剪切层随边处的脉动压力最大,随边角点处脉动压力随相对高度的增加而陡降为0,但腔口导边及侧面处的脉动压力随相对高度增加而略有增大.剪切层自持振荡频率的无量纲数St数随Re变化为一常数值,但其值比气流场中二维陷落腔的St数略大. 相似文献
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针对均匀流场中三维等高型陷落腔因分离流而产生的流激振荡问题开展了系列的实验研究。实验过程中分别考虑了来流攻角为0°和15°时、雷诺数变化范围(Re=2.06.105~1.16.106)时三维等高型陷落腔的流激振荡特性。实验中分别测量了三维腔体侧壁周向及垂向流体压力,在分析腔体内稳态压力和脉动压力的周向、垂向分布规律及腔口剪切层自持振荡特性的基础上,研究了攻角对流体压力分布和剪切层振荡频率特性的影响。实验结果表明:均匀流场中三维陷落腔内部压力分布复杂且当雷诺数大于某值时腔体内稳态压力全都呈现出负压,同时来流攻角的增加使腔口导边、随边和腔体内稳态压力明显地减小,顶流点处的稳态压力随相对高度增加先减小后增大。攻角的增加使剪切层振荡频率减小,但并未影响剪切层振频无量纲St数随流速的变化规律。 相似文献
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In an atrocious ocean environment,the lateral propulsion hole could potentially be partly out of water and capture an air cavity.Bubbles would form when the captured air cavity escapes underwater and they may affect the performance of the sonar.The common commercial computational fluid dynamics software CFX was adopted to calculate the ambient flow field around the lateral propulsion hole generated by a moving vessel.The oscillation of the spherical bubble was based on the Rayleigh-Plesset equation and its migration was modeled using the momentum equation.The radiated noise of the oscillating bubble was also studied.The aim is that the results from this paper would provide some insight into corresponding fluid and acoustic study. 相似文献
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