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空泡尾部流场特性数值模拟研究
引用本文:蒋增辉,于开平,张嘉钟,王聪,黄文虎.空泡尾部流场特性数值模拟研究[J].船舶力学,2008,12(2):225-230.
作者姓名:蒋增辉  于开平  张嘉钟  王聪  黄文虎
作者单位:哈尔滨工业大学航天学院,哈尔滨,150001;哈尔滨工业大学航天学院,哈尔滨,150001;哈尔滨工业大学航天学院,哈尔滨,150001;哈尔滨工业大学航天学院,哈尔滨,150001;哈尔滨工业大学航天学院,哈尔滨,150001
摘    要:使用商用软件FLUENT6.0,对不同的空泡形态下空泡尾部的阻力特性进行了数值模拟研究.研究表明,随着通气率的增大和空泡形态的增长,运动体尾部阻力系数逐渐减小,并且在减小至谷底后又开始回升.尾部压差阻力系数大于粘滞阻力系数,二者均随着通气率的增加而减小.并且压差阻力系数在达到最小值后开始逐渐增大,因而使得总尾部阻力系数在减小至谷底后开始回升.运动体尾部沾湿长度随着通气率的增大而减小,尾部阻力系数则随着尾部沾湿长度的增大而增大.

关 键 词:空泡  阻力特性  数值模拟
文章编号:1007-7294(2008)02-0225-06
修稿时间:2007年8月23日

Numerical simulation on character of the cavity wake region
JIANG Zeng-hui,YU Kai-ping,ZHANG Jia-zhong,WANG Cong,HUANG Wen-hu.Numerical simulation on character of the cavity wake region[J].Journal of Ship Mechanics,2008,12(2):225-230.
Authors:JIANG Zeng-hui  YU Kai-ping  ZHANG Jia-zhong  WANG Cong  HUANG Wen-hu
Abstract:In order to investigate the drag character of the aft section of underwater bodies at the different cavity shapes,numerical investigation was conducted using the commercial CFD software Fluent6.0. The investigation shows with the increasing of ventilation flow rate coefficient and development of cavity,the drag coefficient of the aft section decreases,and then increases when it drops to the minimum. Pressure drag is larger than viscous drag of the aft section,and both decrease when ventilation flow rate coefficient increases.The pressure drag starts to increase when it reaches the minimum,which makes the overall vehicle drag also increases when it reaches the minimum.The wetted length of the aft section decreases with the increasing of ventilation flow rate coefficient,and the drag coefficient of aft section increases when the wetted length increases.
Keywords:cavity  drag character  numerical simulation
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