Abstract

The steady non cavitation hydrodynamic characteristics of CLB4-55-1 tandem propeller and the steady cavitation flows of NACA66 hydrofoil are numerically studied firstly based on the RANS equations of homogeneous multiphase using CFD theory, combined with the SST k-ω turbulent model and Z-G-B cavitation model. Numerical simulation results are in good agreement with the experimental results, which indicates that the numerical method is reliable and accurate. Then, the cavitation performance of the tandem propeller are numerical simulated and analyzed. The results show that the computational model can predict the cavitation performance of tandem propeller accurately. The cavitation performance of tandem propeller is nearly the same as single propeller, however, the cavitation phenomenon of back propeller is greater than the head propeller at certain advance coefficient and cavitation number. The cavitation phenomenon will disappear with the increase of the advance coefficient or the cavitation number.

Highlights

  • The results show that the computational model can predict the cavitation performance of tandem propeller ac⁃ curately

  • Ship Science And Technology, 2014, 36(12) : 11⁃15 ( in Chinese)

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Summary

Introduction

西北工业大学学报 Journal of Northwestern Polytechnical University https: / / doi.org / 10.1051 / jnwpu / 20183630509 摘 要:运用计算流体力学(CFD)理论,基于均质多相流雷诺平均 N⁃S(RANS)方程,结合 SST k⁃ω 湍 流模型及 Z⁃G⁃B (Zwart⁃Gerber⁃Belamri)空化模型,首先对 CLB4⁃55⁃1 串列螺旋桨的非空化定常水动力 特性及对 NACA66 翼型的定常流空化性能进行数值模拟,验证计算方法的可靠性;然后对该串列螺旋 桨的空化性能展开数值模拟与分析。 计算结果表明,所建立数值计算模型可以较为精确地预报串列 螺旋桨的空化性能;串列桨的空化特性相较于单桨基本一致,但是在某些特定进速系数及空化数时, 后桨的空化现象较前桨更为明显;当进速系数变大或空化数变大时,空化现象均会消失。 对于螺旋桨空化特性的研究,主要有实验和数 值模拟 2 种方法,前者耗时耗力且需要一定的实验 条件, 而随着计算机技术的发展, 计算流体力学 ( CFD) 技术蓬勃发展,基于数值模拟技术进行科学 研究已经成为现在的研究主流,而且其具有信息量 全且容易实现的特点,深受研究者们的喜爱。 基于 势流理论及黏流理论,利用面元法及求解 RANS 方 程来数值模拟螺旋桨水动力特性及空化特性的技术 已经日渐成熟,且通过研究者们进行对比,数值计算 结果相当可靠,目前国内外已经取得了很多相关成

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