研究在水面上自由运动的飞行器周围的多相流

V. Pegov, I. Moshkin
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引用次数: 0

摘要

本文对具有垂直工段的大型高速水动力隧道的多相绕流模型进行了实验研究。得到了垂直空腔中阻力系数与空化数的实验关系。考虑了垂直下降流体流动中旋转体周围空化流动的结果。提出了一种基于细长体理论的垂直空腔形状计算方法。对于很长的空腔,得到了适合工程评价的关系式。在非定常空化流中,采用垂直运动模型对水下运动进行了数值模拟。通过确定气腔的非定常边界和水射流尾部的线性载荷,可以计算水动力载荷,并将预测结果与实验数据进行了比较。将分析结果与实验数据进行了对比验证。验证了该方法对确定多相流条件下车辆动力参数的适用性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Studying multiphase flow around a vehicle moving freely to the water surface
The paper provides an experimental study of a multiphase flow around models in a large high-speed hydrodynamic tunnel with a vertical working section. Experimental dependences of drag coefficients on the cavitation number for vertical cavities are obtained. The results of cavitation flow around bodies of revolution in a vertically descending fluid flow are considered. A methodology for calculating the shape of vertical cavities under the slender-body theory is proposed. Relationships suitable for engineering evaluation are obtained for very long cavities. Numerical simulation of underwater motion is performed with models moving vertically in a nonstationary cavitation flow. The hydrodynamic loads can be evaluated through the determination of the nonstationary boundaries of a gas cavity and a linear load on a water-flown aft. The predicted results are compared with the experimental data. Validation and verification are performed by comparing the analysis results with the experimental data. The applicability of the proposed method to the determination of the hydrodynamic parameters of vehicles under multiphase flow is demonstrated.
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