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首页> 外文期刊>Experimental Thermal and Fluid Science: International Journal of Experimental Heat Transfer, Thermodynamics, and Fluid Mechanics >Effect of mounting strut and cavitator shape on the ventilation demand for ventilated supercavitation
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Effect of mounting strut and cavitator shape on the ventilation demand for ventilated supercavitation

机译:安装支柱和空穴形状对通风超渗流通风需求的影响

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摘要

The present work systematically investigates the effect of cavitator mounting strut and cavitator shape on the ventilation demand to form and sustain a ventilated supercavity under different flow conditions. Three cavitators of different shapes (i.e. 2D cavitators including triangle and disk shape, and 3D cone-shaped cavitator) with the same frontal area are employed for the experiments. The cavitator is connected to a ventilation pipe extended upstream from a mounting strut, referred to as forward-facing model (FFM). The minimal ventilation coefficients to generate (C-Qf) and to collapse (C-Qc) a supercavity are measured over a wide range of Froude number (Fr) for each cavitator. Images of overall cavity shapes and topology near closure region as well as the cavity pressure under different experimental conditions are captured simultaneously. The results are compared across different cavitator shapes and the disk cavitator situated on the downstream side of the mount strut, referred to as backward-facing model (BFM). Similar C-Qf - Fr curves were observed in BFM and FFM-configured disk cavitators. The cone-shaped cavitator requires the least amount of ventilation to generate a supercavity among all different shapes across the range of Fr in our experiments. The C-Qc of disk FFM is lower than that of its BFM counterpart at small Fr and exceeds the BFM C-Qc with further increase of Fr. The cone cavitator has the smallest C-Qc among all the cavitators across the range of Fr in our experiments. To elucidate the trends of C-Qc upon changing Fr and cavitator shape, the geometry of supercavity under C-Qc including its overall shape, the cavity maximum diameter (D-max) and half length (L-1/2) are also investigated. Both D-max and L-1/2 show an increasing then plateauing trend upon increasing Fr across different FFM cavitators despite the smaller values for the 3D cone cavitator. Subsequently, such cavity geometric information and cavity pressure measurements in conjunction with high speed imaging of re-entrant jet are employed to estimate the re-entrant jet momentum under different Fr for disk and cone cavitators. The estimated re-entrant jet momentum shows reasonable match with the ventilation air momentum under C-Qc in lower Fr for both cavitator cases, with the disk cavitator case yielding significantly stronger re-entrant jet, providing support to the re-entrant jet mechanism governing on the cavity collapse. Our study sheds some light on the cavitator design and ventilation strategy for a supercavitating vehicle in practice.
机译:本工作系统地研究了空腔安装支柱和空腔形状对通风需求的影响,以在不同的流动条件下形成和维持通风的超障碍。实验采用具有相同正面区域的不同形状(包括三角形和盘形和3D锥形空腔)的三个不同形状的空穴器,用于实验。空穴能器连接到从安装支柱上游的通风管道,称为面向前部模型(FFM)。产生(C-QF)和折叠(C-QC)的最小通风系数在每个空穴器的各种FRoude数(FR)上测量超级避险度。同时捕获封闭区域附近的整体腔形状和拓扑结构的图像以及腔压力的图像。将结果与位于安装支柱的下游侧的不同的空穴形状和盘空穴器中进行比较,称为后向朝向模型(BFM)。在BFM和FFM配置的盘空穴器中观察到了类似的C-QF - FR曲线。锥形空腔需要最少量的通风,以在我们的实验中的FR范围内产生所有不同形状的超级避险度。磁盘FFM的C-QC低于小FF的BFM对应物的C-QC,超过BFM C-QC,进一步增加了FR.在我们的实验中,锥形空穴在所有空体中都有最小的C-QC。为了在改变FR和空腔形状时阐明C-QC的趋势,C-QC下超级沟壑的几何形状还研究了其整体形状,腔最大直径(D-MAX)和半长(L-1/2) 。 D-MAX和L-1/2都显示出在不同FFM空穴空穴中越来越多的FFM空穴传输时增加的平台趋势,尽管3D锥形空穴器的值较小。随后,使用重新参赛者射流的高速成像的这种腔几何信息和腔压测量来估计用于盘和锥形空穴的不同FR下的再参赛者喷射动量。估计的再参赛者喷气机动量显示出合理的匹配,在C-QC下的用于空体型情况下的C-QC下的通风气动量匹配,磁盘空腔外壳产生明显更强的再参与者射流,为再参赛喷射机构提供支持在腔坍塌。我们的研究在实践中,在实践中的空穴设计和通风策略上阐明了一些光。

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