超空泡航行体控制面与主空泡相互作用分析

doi:10.3969/j.issn.1000-1093.2017.05.015

摘要/Abstract

摘要： 基于有限体积法，采用均相流模型和流体体积方法开展超空泡航行体在不同空泡流型及不同控制面舵角情况下空化流场数值模拟，研究穿刺空泡情况下超空泡航行体尾部控制面与航行体主空泡之间的相互作用。数值模拟结果表明：航行体主空泡对控制面的影响表现为不同流型下控制面沾湿深度不同，沾湿深度变化量最大可达50%以上，控制面流体动力受沾湿深度影响明显；航行体尾部控制面对主空泡闭合有迟滞作用，主空泡长度平均增量约为3%，控制面存在舵角时将会引起控制面之后的航行体主空泡形态变化，可引起航行体出现不对称沾湿面，且尾部闭合流型受影响最大。因此，超空泡航行体空泡流型设计与控制律设计时应充分考虑控制面与航行体主空泡之间的相互作用。

关键词: 流体力学, 超空泡航行体, 空泡流型, 控制面, 空泡, 相互作用

Abstract: The homogeneous multiphase model and volume of fluid (VOF) method are used to simulate the interaction between control surface and main cavity of supercavitaing vehicle (SCV) under different flow patterns of cavity and angles of attack of control surface. Numerical result shows that the vehicle cavity shape affects the submersion depth of the control surfaces, and the variation of submersion depth is up to above 50 percent. The hydrodynamics of control surface is obviously affected by the variation of submersion depth. The length of main cavity is enlarged by 3 percent in average due to the presence of control surface, the cross shape of main cavity could be significantly changed when there is an angle of attack of the control faces, and the cavity shape of SCV experienced a worst deformation under a base closure cavity flow pattern. The interaction between control surface and main cavity of supercavitating vehicle should be taken into consideration during the design process of cavity flow pattern and control law. Key

Key words: fluidmechanics, supercavitatingvehicle, cavityflowpattern, controlsurface, cavity, interaction

中图分类号:

TJ630.1

周后村，向敏，张为华. 超空泡航行体控制面与主空泡相互作用分析[J]. 兵工学报, 2017, 38(5): 949-958.

ZHOU Hou-cun， XIANG Min， ZHANG Wei-hua. Numerical Research on Interaction between Control Surfaces and Main Cavity of Supercavitating Vehicles[J]. Acta Armamentarii, 2017, 38(5): 949-958.

参考文献

［1］ Kuklinski R, Henoch C, Castano J. Experimental study of ventilated cavities on dynamic test model[C]∥Proceedings of the 4th International Symposium on Cavitation. Pasadena, CA, US: California Institute of Technology, 2001.
[2] 刘淮, 韩雪松, 雷贺攻. 国外高速水下武器技术发展现状及趋势研究[R]. 北京:中国船舶工业综合技术经济研究院, 2008.
LIU Huai, HAN Xue-song, LEI He-gong. Research on current status and trends of high speed undersea weapon technology on the world[R]. Beijing: China Institute of Marine Technology & Economy, 2008.(in Chinese)
[3] 刘喜莹, 张庆明. 超空泡技术研究进展[C]∥中国力学学会学术大会2005论文摘要集. 北京:北京工业大学, 2005.
LIU Xi-ying, ZHANG Qing-ming. Recent research and development in supercavitating technology[C]∥Proceedings of Chinese Conference of Theoretical and Applied Mechanics 2005. Beijing: Beijing University of Chemical Technology, 2005.(in Chinese)
[4] 杨洪澜, 张嘉钟, 赵存宝, 等. 楔体外部超空泡形状预测[J]. 哈尔滨理工大学学报, 2006, 11(4):106-110.
YANG Hong-lan, ZHANG Jia-zhong, ZHAO Cun-bao, et al. Prediction of wedge's supercavity shape[J]. Journal of Harbin University of Science and Technology, 2006, 11(4):106-110.(in Chinese)
[5] 张治勇, 杨洪澜, 张嘉钟. 楔形体诱导的非定常超空泡计算[J]. 工程力学, 2008, 25(8):42-47.
ZHANG Zhi-yong, YANG Hong-lan, ZHANG Jia-zhong. Calculation of unsteady supercavity induced by wedges[J]. Engineering Mechinics, 2008, 25(8): 42-47.(in Chinese)

[6] 裴譞, 张宇文, 袁绪龙, 等. 尾翼对超空泡航行器形态及力学特性影响实验研究[J]. 实验流体力学, 2011, 25(1):23-28.
PEI Xuan, ZHANG Yu-wen, YUAN Xu-long, et al. Exploring experimentally effect of tail wing on shape and dynamics characteristics on super-cavitation vehicle[J]. Journal of Experiments in Fluid Mechanics, 2011, 25(1):23-28. ( in Chinese)
[7] 裴譞, 王育才, 张宇文, 等. 超空泡航行器舵效的水洞试验研究[J]. 西南交通大学学报, 2011, 46(6):1008-1018.
PEI Xuan, WANG Yu-cai, ZHANG Yu-wen, et al. Experimental research on tail rudder efficiency of super-cavitation vehicle[J]. Journal of Southwest Jiaotong University, 2011, 46(6):1008-1018.(in Chinese)
[8] 邢彦江, 张嘉钟, 曹伟, 等. 尾翼楔角对通气超空泡特性影响试验研究[J]. 哈尔滨工业大学学报, 2013, 45(1):25-29.
XING Yan-jiang, ZHANG Jia-zhong, CAO Wei, et al. Experimental investigation of the effect of tail wings wedge angle on ventilated supercavity hydrodynamic[J]. Journal of Harbin Institute of Technology, 2013, 45(1):25-29.(in Chinese)
[9] 张木, 易文俊, 谭俊杰, 等. 带尾翼水下自然超空泡射弹数值模拟研究[J]. 计算力学学报, 2013, 30(1):161-165.
ZHANG Mu, YI Wen-jun, TAN Jun-jie, et al. Numerical investigation of underwater natural supercavitating projectiles operating with the empennages[J]. Chinese Journal of Computational Mechanics, 2013, 30(1):161-165. (in Chinese)

[10] 熊天红, 张木, 易文俊, 等. 带尾翼水下航行体超空泡流数值模拟研究[J]. 弹道学报, 2013, 25(4):43-47.
XIONG Tian-hong, ZHANG Mu, YI Wen-jun, et al. Research on numerical simulation of supercavity flow around Underwater wing-vehicle[J]. Journal of Ballistics, 2013, 25(4):43-47.(in Chinese)
[11] 周清强. 带尾翼通气超空泡航行体流体动力数值模拟[D]. 哈尔滨: 哈尔滨工业大学, 2013.
ZHOU Qing-qiang. Numerical simulation of hydrodynamic characteristics of underwater supercavitation vehicle with fins[D]. Harbin: Harbin Institute of Technology, 2013.(in Chinese)
[12] 张宇文, 袁绪龙, 邓飞. 超空泡航行体流体动力学[M]. 北京: 国防工业出版社, 2014.
ZHANG Yu-wen, YUAN Xu-long, DENG Fei. Fluid dynamics of supercavitating underwater vehicles[M]. Beijing: National Defense Industry Press, 2014.(in Chinese)

[13] Kirschner I N, Kring D C, Stokes A W, et al. Control strategies for supercavitating vehicles[J]. Journal of Vibration and Control, 2002, 8(2):219-242.
[14] Goel A. Robust control of supercavitating vehicles in the presence of dynamic and uncertain cavity[D]. FL, US: University of Florida, 2005.
[15] Vanek B. Control methods for high-speed supercavitating vehicles[D]. MN, US: University of Minnesota, 2008.
[16] 林明东. 超高速鱼雷总体技术研究[D]. 长沙: 国防科学技术大学, 2012.
LIN Ming-dong. Research on conceptual design technologies of ultrahigh speed torpedo[D]. Changsha: National University of Defense Technology, 2012.(in Chinese)

[17] 王雨. 水下高速航行体航向控制技术研究[D]. 哈尔滨:哈尔滨工程大学, 2012.
WANG Yu. Research on course motion control of underwater high speed vehicle[D]. Harbin: Harbin Engineering University, 2012.(in Chinese)

[18] 王志学. 水下高速航行体纵向控制研究[D]. 哈尔滨: 哈尔滨工程大学, 2013.
WANG Zhi-xue. Research on longitudinal control of underwater high speed vehicle[D]. Harbin: Harbin Engineering University, 2013.(in Chinese)

[19] Zou W, Yu K P, Arndt R. Modeling and simulations of supercavitating vehicle with planing force in the longitudinal plane[J]. Applied Mathematical Modelling, 2015, 39(19):6008-6020.
[20] Escobar D, Vollmer D, Arndt R. Modeling, control, and experimental validation of a high-speed supercavitating vehicle[J]. IEEE Journal of Oceanic Engineering, 2015, 40(2):362-373.
[21] Escobar D. Modeling, robust control, and experimental validation of a supercavitating vehicle[D]. MN, US:University of Minnesota, 2015.
[22] Escobar D, Vollmer D, Arndt R. A dynamic testbed for supercavitating vehicle control[J]. Journal of Physics: Conference Series, 2015, 656:012144.
[23] 栗夫园, 张宇文, 滕鹏桦，等. 超空泡鱼雷外形优化[J]. 北京航空航天大学学报, 2014, 40(6):815-818.
LI Fu-yuan, ZHANG Yu-wen, TENG Peng-hua, et al. Shape optimizaiton of supercavitating torpedo[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(6): 815-818.(in Chinese)
[24] 周后村. 超空泡航行体流体外形设计及水动力特性分析[D]. 长沙: 国防科学技术大学, 2015.
ZHOU Hou-cun.Hydrodynamic configuration design and hydrodynamic characteristics analysis of supercavitating vehicles[D]. Changsha: National University of Defense Technology, 2015.(in Chinese)
[25] Wosnik M, Arndt R E A. Control experiments with a semi-axisymmetric supercavity and a supercavity piercing fin[C]∥7th International Symposium on Cavitation. Ann Arbor, MI, US: University of Michigan, 2009.

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2017 年5月兵工学报ACTA
ARMAMENTARIIVol.38No.5May2017

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