...
首页> 外文期刊>Chemical Engineering Science >Numerical analysis on cavitation effects in submerged water jet added with turbulent drag-reducing additives of CTAC
【24h】

Numerical analysis on cavitation effects in submerged water jet added with turbulent drag-reducing additives of CTAC

机译:用CTAC湍流阻力减少添加剂添加淹没水射流空化效应数值分析

获取原文
获取原文并翻译 | 示例
           

摘要

In this paper the cavitation phenomenon and bubble collapse in submerged water jet added with CTAC were studied. The cavitation simulation was based on an improved cavitation model established by introducing coefficients into traditional cavitation model. The coefficients were obtained by fitting the numerical solutions of Rayleigh-Plesset equation in which the viscosity term and surface tension term were not neglected. Cross model was also employed to express the shear-thinning character of the surfactant solution. Simulation results show that the whole cavitation intensity decreased but the scale of cavitation region increased in drag-reducer solution. The submerged water jet added with drag-reducer was less dispersed and the stagnation pressure near the wall was significantly improved. Simulation results of the bubble collapse process show that the bubble collapsed more slowly in drag-reducer solution in comparison with that in pure water. The two pressure peaks near the wall during the collapse process appeared later in drag-reducer solution and the maximum value of the pressure generated in drag-reducer solution was less than that in pure water. (C) 2018 Elsevier Ltd. All rights reserved.
机译:本文研究了CTAC加入淹没水射流中的空化现象和泡沫塌陷。空化模拟基于通过将系数引入传统的空化模型来建立的改进的空化模型。通过拟合瑞利 - Plesset方程的数值解来获得系数,其中粘度术语和表面张力术语未被忽略。还用于表达表面活性剂溶液的剪切变薄特征的交叉模型。仿真结果表明,整个空化强度下降,但阻力区溶液中的空化区域规模增加。添加用拖减速器的浸没式水射流较少分散,墙上附近的停滞压力显着改善。泡沫塌陷过程的仿真结果表明,与纯水相比,泡沫在阻力溶液中坍塌更慢。在坍塌过程中靠近壁附近的两个压力峰值后来出现在阻力 - 减速器溶液中,并且在阻力 - 减速剂溶液中产生的压力的最大值小于纯水中的压力。 (c)2018年elestvier有限公司保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号