Volume 23 Issue 2
Feb.  2008
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CHEN Yang, GAO Fang, ZHANG Zhen-peng, WANG Hai-xing, CAI Guo-biao. Finite volume model for quasi one-dimensional compressible transient pipe flow (Ⅱ) Finite volume model of temperature field[J]. Journal of Aerospace Power, 2008, 23(2): 317-322.
Citation: CHEN Yang, GAO Fang, ZHANG Zhen-peng, WANG Hai-xing, CAI Guo-biao. Finite volume model for quasi one-dimensional compressible transient pipe flow (Ⅱ) Finite volume model of temperature field[J]. Journal of Aerospace Power, 2008, 23(2): 317-322.

Finite volume model for quasi one-dimensional compressible transient pipe flow (Ⅱ) Finite volume model of temperature field

  • Received Date: 2007-01-15
  • Rev Recd Date: 2007-03-28
  • Publish Date: 2008-02-28
  • Based on the flow field model,a finite volume model suitable for simulating pipe wall transient heat transfer was established by employing two-dimensional finite control volume grids in axisymmetric cylindrical coordinates which can deal with two boundary heat transfer conditions including convection and radiation.Variable thermophysical properties of wall material and multilayer or vacuum sandwich structure of pipe wall were also considered.The temperature field model is a natural extension of flow field modeling method.The union of both forms the finite volume model(FVM) of quasi one-dimensional compressible transient pipe flow,which is a uniform numerical system of flow and heat transfer.Furthermore, combing with throttling model of valve core,the model can be further developed to establish the flow field and temperature field models of common components in pipe system.The modeling and simulation of a certain liquid rocket engine test-bed LO2 tank pressurization system shows that the FVMhas a wide scope of application and good simulation precision.

     

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  • [1]
    陈阳.液体火箭发动机试验台气路系统通用模块化建模与仿真研究[D].北京:北京航空航天大学,2006.
    [2]
    陈阳,高芳,张振鹏,等.准一维可压缩瞬变管流的有限体积模型(Ⅰ)流场的有限体积模型[J].航空动力学报,2008,23(2):311-316.CHEN Yang,GAO Fang,ZHANG Zhenpeng,et al.Finite volume model for quasi one-dimensional compressible transient pipe flow(Ⅰ)Finite volume model of flow field[J].Journal of Aerospace Power,2008,23(2):311-316.
    [3]
    张育林,刘昆,程谋森.液体火箭发动机动力学理论与应用[M].北京:科学出版社,2005.
    [4]
    刘昆,程谋森,张育林.低温推进剂供应管道系统充填过程的动力学模型[J].国防科技大学学报,2003,25(3):1-5.LIU Kun,CHENG Mousen,ZHANG Yulin.Dynamic model of priming processes of cryogenic propellant feed lines[J].Journal of National University of Defense Technology,2003,25(3):1-5.
    [5]
    Cullimore B A,Beer C M,Johnson D A.Propulsion applications of the NASA standard general purpose thermohydraulic analyzer[R].AIAA2000-3723,2000.
    [6]
    Schallhorn P A,Palmiter C,Farmer J,et al.Interfacing the generalized fluid system simulation program with the SINDA/G thermal program[R].AIAA2000-2504,2000.
    [7]
    (美)Partankar S V.传热与流体流动的数值计算[M].张政,译.北京:科学出版社,1984.
    [8]
    王补宣.工程传热传质学[M].北京:科学出版社,1998.
    [9]
    (美)Karlekar B V,Desmond R M.工程传热学[M].刘吉萱,译.北京:人民教育出版社,1981.
    [10]
    杨世铭.传热学[M].北京:高等教育出版社,1987.
    [11]
    朱谷君.工程传热传质学[M].北京:航空工业出版社,1989.
    [12]
    钱滨江,伍贻文,常家芳,等.简明传热手册[M].北京:高等教育出版社,1983.
    [13]
    陈阳,张振鹏,瞿骞,等.液体火箭发动机试验台贮箱增压系统数值仿真[J].航空动力学报,2007,22(1):96-101.CHEN Yang,ZHANG Zhenpeng,QU Qian,et al.Numerical simulation for tank pressurization system of LRE testbed[J].Journal of Aerospace Power,2007,22(1):96-101.
    [14]
    翟骞.高压、小气枕低温贮箱智能增压技术[J].低温工程,2005,(5):22-25.QU Qian.An intelligence pressurization technology of high pressure and small ullage at low temperature Tank[J].Cryogenics,2005,(5):22-25.
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