Volume 32 Issue 6
Jun.  2017
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Dynamic characteristics of fluid-filled pipe in liquid rocket engines considering fluid-structure interaction[J]. Journal of Aerospace Power, 2017, 32(6): 1523-1529. doi: 10.13224/j.cnki.jasp.2017.06.030
Citation: Dynamic characteristics of fluid-filled pipe in liquid rocket engines considering fluid-structure interaction[J]. Journal of Aerospace Power, 2017, 32(6): 1523-1529. doi: 10.13224/j.cnki.jasp.2017.06.030

Dynamic characteristics of fluid-filled pipe in liquid rocket engines considering fluid-structure interaction

doi: 10.13224/j.cnki.jasp.2017.06.030
  • Received Date: 2016-03-06
  • Publish Date: 2017-06-28
  • To study the influence of fluid-structure interaction (FSI) on the frequency characteristics of fluid-filled pipe in rocket engines, a dynamic characteristic model of spatial pipe was set up based on transfer matrix method(TMM). Targeting a real liquid rocket engine pipe, simulations by transfer matrix method as well as conventional finite element method (FEM) for fluid with added-mass (non-FSI) were proposed, and verification modal test was also carried out. Influences of parameters such as diameter and thickness of the pipe on the coupling effect were discussed. The results indicate that each resonant frequency declines and the corresponding amplitude increases under FSI effect. In addition, the influence of pipe thickness on low-order resonant frequencies is more significant than the pipe diameter. The example given hereto also demonstrate that the concerned 1st-order resonant frequency calculated by the non-FSI model offsets is over 10% when the pipe thickness exceeds 30% of the design value, so the coupling effect can not be ignored in this case. And the influence of pipe thickness on 1st-order resonant frequency is less than 8% within the range of calculation.

     

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  • [1]
    徐云飞.基于流固耦合的火箭发动机导管振动特性研究[D].西安:西安航天动力研究所,2009.XU Yunfei.Vibration characteristic study of rocket engine pipe based on fluid-structure interaction[D].Xian:Xian Aerospace Propulsion Institute,2009.(in Chinese)
    [2]
    休泽尔.液体火箭发动机现代工程设计[M].朱宁昌,译.北京:中国宇航出版社,2004.
    [3]
    李斌,杜大华.液氧/煤油补燃发动机低频频率特性研究[J].航空动力学报,2009,24(5):1187- 1191.LI Bin,DU Dahua.Research on the low frequency characteristics of LOX/kerosene stage combustion cycle engine[J].Journal of Aerospace Power,2009,24(5):1187-1191.(in Chinese)
    [4]
    陈香林,周文禄.压力管道流固耦合振动特性[J].火箭推进,2007,33(5):27-31.CHEN Xianglin,ZHOU Wenlu.Vibration characteristic analysis of pressure pipes with fluid-structure interaction[J].Journal of Rocket Propulsion,2007,33(5):27-31.(in Chinese)
    [5]
    HIREMATH S S.Modeling and simulation of fluid structure interaction in jet pipe electrohydraulic servovalve[J].International Journal of Recent Advances in Mechanical Engineering,2013,2(4):1-14.
    [6]
    GIM G,CHANG S,LEE S,et al.Fluid-structure interaction in a U-tube with surface roughness and pressure drop[J].Nuclear Engineering and Technology,2014,46(5):633-640.
    [7]
    TIJSSELING A S.Exact computation of the axial vibration of two coupled liquid-filled pipes[R].ASME Paper PVP2009-77250,2009.
    [8]
    魏鑫,孙冰,于子文,等.火箭推进系统充液管路的流固耦合动响应分析[J].航空动力学报,2010,25(4):852-856.WEI Xin,SUN Bing,YU Ziwen,et al.Dynamic response analysis of fluid-structure interaction in liquid-filled pipes of rocket feed system[J].Journal of Aerospace Power,2010,25(4):852-856.(in Chinese)
    [9]
    KERAMAT A,TIJSSELING A S,HOU Q,et al.Fluid-structure interaction with pipe-wall viscoelasticity during water hammer[J].Journal of Fluid and Structures,2012,28(1):434-455.
    [10]
    张智勇,沈荣瀛,王强.充液管道系统的模态分析[J].固体力学学报,2001,22(2):143-149.ZHANG Zhiyong,SHEN Rongying,WANG Qiang.The modal analysis of the liquid-filled pipe system[J].Chinese Journal of Solid Mechanics,2001,22(2):143-149.(in Chinese)
    [11]
    张立翔,杨柯.流体结构互动理论及其应用[M].北京:科学出版社,2004.
    [12]
    YANG Ke,LI Q S,ZHANG Lixiang.Longitudinal vibration analysis of multi-span liquid-filled pipelines with rigid constraints[J].Journal of Sound and Vibration,2004,273(1/2):125-147.
    [13]
    MOLINSKY J.Water hammer test of the seastar hydrazine propulsion system[R].AIAA 97-3226,1997.
    [14]
    PRICKETT R P,MAYER E,HERMEL J,et al.Water hammer in a spacecraft propellant feed system[R].AIAA 88-2920,1988.
    [15]
    LECOURT R,STEELANT J.Experimental investigation of waterhammer in simplified basic pipes of satellite propulsion systems[R].AIAA-2007-5532,2007.
    [16]
    张智勇,沈荣瀛.充液直管管系中的固-液耦合振动响应分析[J].振动工程学报,2000,13(3):455-461.ZHANG Zhiyong,SHEN Rongying.Fluid-structure interaction of the straight liquid-filled piping system[J].Journal of Vibration Engineering,2000,13(3):455-461.(in Chinese)
    [17]
    杨超,范士娟.管材参数对输液管流固耦合振动的影响[J].振动与冲击,2011,30(7):210-213.YANG Chao,FAN Shijuan.Influence of pipe parameters on fluid-structure coupled vibration of a fluid-conveying pipe[J].Journal of Vibration and Shock,2011,30(7):210-213.(in Chinese)
    [18]
    JONG C D.Analysis of pulsations and vibrations in fluid-filled pipe systems[D].Eindhoven,Holland:Eindhoven University of Technology,1994.
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