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通气位置对潜射航行体流体动力特性影响分析

孙铁志 魏英杰 王聪 曹伟

孙铁志, 魏英杰, 王聪, 等 . 通气位置对潜射航行体流体动力特性影响分析[J]. 北京航空航天大学学报, 2013, 39(10): 1303-1308.
引用本文: 孙铁志, 魏英杰, 王聪, 等 . 通气位置对潜射航行体流体动力特性影响分析[J]. 北京航空航天大学学报, 2013, 39(10): 1303-1308.
Sun Tiezhi, Wei Yingjie, Wang Cong, et al. Analysis of the effect of ventilation positions on hydrodynamic characteristics of submarine-launched vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(10): 1303-1308. (in Chinese)
Citation: Sun Tiezhi, Wei Yingjie, Wang Cong, et al. Analysis of the effect of ventilation positions on hydrodynamic characteristics of submarine-launched vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(10): 1303-1308. (in Chinese)

通气位置对潜射航行体流体动力特性影响分析

基金项目: 中央高校基本科研业务费专项资金资助项目(HIT.NSRIF.201159); 哈尔滨市科技创新人才研究专项资金项目(2013RFLXJ007)
详细信息
    作者简介:

    孙铁志(1986-),男,吉林洮南人,博士生,hitstzjg@163.com.

  • 中图分类号: TJ762.4

Analysis of the effect of ventilation positions on hydrodynamic characteristics of submarine-launched vehicle

  • 摘要: 基于均质平衡流理论,通过求解混合介质的RANS方程、SST湍流输运方程和各相之间的质量输运方程,开展了通气位置对潜射航行体流体动力特性影响的三维数值模拟研究,对比分析了不同通气位置条件下空泡形态特性、表面压力分布以及阻力变化特性.结果表明:当两个通气口间距增加到一定值后,在两个通气口之间区域空泡发生断裂,在断裂区域迎流面和背流面表面压力值升高,且在空泡断裂闭合位置出现压力峰值;在相同通气量条件下,随着通气口间距的增大,压差阻力系数和粘性阻力系数均呈减小趋势变化.

     

  • [1] Savchenko Y N.Control of supercavitation flow and stability of supercavitating motion of bodies [C/OL].RTO AVT/VKI Special Course:Supercavitating Flows,von Karman Institute for Fluid Dynamics,Rhode-Saint-Genese,Belgium.2001:12-16 [2] Reichardt H.The laws of cavitation bubbles as axially symmetrical bodies in a flow[C]//Ministry of Aircraft Productuin (Great Britian),Reports and Translations,1946(766):322-326 [3] Silberman E,Song C S.Instability of ventilated cavities[J].Journal of Ship Research,1961,5(1): 13-33 [4] Lindau J W,Kunz R F,Mulherin J M,et al.Fully coupled 6-DOF to URANS modeling of cavitating flows around a supercavitating vehicle[C]//Fifth International Symposium on Cavitation (CAV2003) .Osaka,Japan: ,2003 [5] 张学伟,张亮,张嘉钟,等.通气超空泡稳定性分析的一种数值算法[J].力学学报,2008,40(6):820-825 Zhang Xuewei,ZhangLiang,Zhang Jiazhong et al.Numerical method for the stability analysis of ventilated supercavity[J].Chinese Journal of Theoretical and Applied Mechanics,2008, 40(6): 820-825 (in Chinese) [6] Acosta A J.The effect of a longitudinal gravity field on the supercavitating flow over a wedge [J].Trans ASME,1961,28(2): 188-192 [7] Kawakami.Investigation of the behavior of ventilated supercavities[C]//American Society of Mechanical Engineers,Fluids Engineering Division FEDSM.2010:57-64 [8] Matveev K I,Miller M J.Air cavity with variable length under model hull[J].Journal of Engineering for the Maritime Environment,2011,225(2):161-169 [9] 刘筠乔,鲁传敬,李杰,等.导弹垂直发射出筒过程中通气空泡流研究[J].水动力研究与进展,2007,22(5): 549-554 Liu Yunqiao,Lu Chuanjing,Li Jie.An investigation of ventilated cavitating flow in vertical launching of a missile[J].Journal of Hydrodynamics,2007,22(5): 549-554(in Chinese) [10] 闵景新,魏英杰,王聪,等.潜射导弹垂直发射过程流体动力特性数值模拟[J].兵工学报,2010,31(10):1303-1309 Min Jingxin,Wei Yingjie,Wang Cong,et al.Numerical simulation on hydrodynamic characteristics of submarine missile in the verticallaunch process[J].Acta Armamentarii,2010,31(10): 1303-1309(in Chinese) [11] Ramesh S S,Lim K M,Khoo B C.An axisymmetric hypersingular boundary integral formulation for simulating acoustic wave propagation in supercavitating flows[J].Journal of Sound and Vibration,2012,3(31): 4313-4342 [12] Menter F R.Two-equation eddy-viscosity turbulence models for engineering applications[J].AIAA-Journal,1994,32(8): 1598-1605 [13] Rouse H,McNown J S.Cavitation and pressure distribution,head forms at zero angle of yaw[R].State University of Iowa Engineering Bulletin 32,No.420,1948
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出版历程
  • 收稿日期:  2013-01-04
  • 网络出版日期:  2013-10-30

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