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基于Logvinovich独立膨胀原理的超空泡形态计算方法
引用本文:张学伟,张亮,王聪,张嘉钟,魏英杰.基于Logvinovich独立膨胀原理的超空泡形态计算方法[J].兵工学报,2009,30(3):361-365.
作者姓名:张学伟  张亮  王聪  张嘉钟  魏英杰
作者单位:哈尔滨工程大学,深海工程技术研究中心,黑龙江,哈尔滨,150001;哈尔滨工业大学,航天学院,黑龙江,哈尔滨,150001
基金项目:高等学校学科创新引智计划 
摘    要:根据Logvinovich独立膨胀原理发展了一种用于计算定常、非定常自然和通气超空泡形态的计算方法。运用该方法对在圆盘空化器速度和流场压力扰动下的自然和通气超空泡非定常变化过程进行了数值仿真,结果表明:自然超空泡在非定常和准定常条件下的形态特性存在较大差别,超空泡长度变化相对于非定常扰动表现出时间滞后性;通气超空泡与自然超空泡形态特性也存在差别,通气超空泡在非定常扰动下的过渡时间较长,振动幅度较大。

关 键 词:流体力学  自然超空泡  通气超空泡  独立膨胀原理  非定常计算方法

A Calculation Method for Supercavity Shape Based on the Logvinovich Independence Principle of the Cavity Section Expansion
ZHANG Xue-wei,ZHANG Liang,WANG Cong,ZHANG Jia-zhong,WEI Ying-jie.A Calculation Method for Supercavity Shape Based on the Logvinovich Independence Principle of the Cavity Section Expansion[J].Acta Armamentarii,2009,30(3):361-365.
Authors:ZHANG Xue-wei  ZHANG Liang  WANG Cong  ZHANG Jia-zhong  WEI Ying-jie
Affiliation:I. Deepwater Engineering Research Center, Harbin Engineering University, Harbin 150001, Heilongjiang, China; 2. School of Astronautics, Harbin Institute of Technology, Harbin 150001, Heilongjiang, China
Abstract:A calculation method was brought forward to calculate steady and unsteady natural and ven?tilated supercavities based on the Logvinovich principle of the cavity sections expansion. Unsteady nat?ural and ventilated supercavities disturbed with the changes of disk cavitator velocity and flowfield pressure were simulated by the method. The simulated results indicate that the shape characteristic of quasi-steady natural supercavity is distinct from that of unsteady natural supercavity, the change of un?steady supercavity length lags behind disturbances; the shape characteristic of natural supercavity is al?so distinct from that of ventilated supercavity, ventilated supercavity has longer transition time and larger oscillating amplitude than those of natural supercavity under unsteady disturbance.
Keywords:fluid mechanics    natural supercavity    ventilated supercavity    principle of Logvinovich of the cavity sections expansion    unsteady calculating method  
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