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Volume 40 Issue 3
Mar.  2014
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Journal of Beijing University of Aeronautics and Astronautics  > 2014  >  40(3): 417-421.
Yang Jianlong, Liu Meng. Influence of limiters on numerical simulation of heating distributions for hypersonic bodies[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 417-421. doi: 10.13700/j.bh.1001-5965.2013.0253(in Chinese)
Citation: Yang Jianlong, Liu Meng. Influence of limiters on numerical simulation of heating distributions for hypersonic bodies[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 417-421. doi: 10.13700/j.bh.1001-5965.2013.0253(in Chinese)
shu

Influence of limiters on numerical simulation of heating distributions for hypersonic bodies

doi: 10.13700/j.bh.1001-5965.2013.0253

  • School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 10 May 2013
  • Publish Date: 20 Mar 2014
    Abstract
  • The Roe's flux difference splitting (FDS) scheme was combined with min mod, van Leer and Osher-C limiters to simulate hypersonic flow fields around hypersonic bodies. The different effects of the three limiters on the simulation results of hypersonic bodies' aerodynamics and aerothermodynamics were researched, and their effects on the simulation of heating rates were compared and analyzed. From the results, it can draw the following conclusions: the choice of limiters has a very important effect on numerical simulation results, and it will influence the simulation results of aerothermodynamics more than the ones of aerodynamics. The min mod limiter, working together with Roe's FDS scheme can obtain better heating rates on hypersonic bodies than the other two limiters no matter for simple or complex aerodynamic shapes. Therefore, the min mod limiter can provide reliable results for the thermal protection designs.

     

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    • References(18)
  • [1]
    钱翼稷.空气动力学[M].北京:北京航空航天大学出版社,2004:362-383 Qian Yiji.Aerodynamics[M].Beijing:Beihang University Press,2004:362-383(in Chinese)
    [2]
    王浚,王佩广.高超声速飞行器一体化防护与热控制设计方法[J].北京航空航天大学学报,2006,32(10):1130-1134 Wang Jun,Wang Peiguang.Integrated thermal protection and control system design methodology for hypersonic vehicles[J].Journal of Beijing University of Aeronautics and Astronautics,2006,32(10):1130-1134(in Chinese)
    [3]
    阎超.计算流体力学方法及应用[M].北京:北京航空航天大学出版社,2006:123-130 Yan Chao.Computational fluid dynamics methods and applications[M].Beijing:Beihang University Press,2006:123 -130(in Chinese)
    [4]
    Scott J N,Niu Y Y.Comparison of limiters in flux-split algorithms for Euler equations[R].AIAA Paper 93-0068,1993
    [5]
    Druguet M C,Candler G V,Nompelis I.Effect of numeric on Navier-Stokes computation of hypersonic double-cone flows[J].AIAA Journal,2005,43(3):616-623
    [6]
    Li Q B,Fu S,Xu K.Application of gas-kinetic scheme with kinetic boundary conditions in hypersonic flow[J].AIAA Journal,2005,43(10):2170-2176
    [7]
    Kitamura K,Nishino A,Ishikawa T,et al.A device for reduction of heat flux produced by hypersonic shock interference[R].AIAA Paper 2004-2638,2004
    [8]
    Chan J,Sislian J P,Alexander D.Numerically simulated comparative performance of a scramjet and shcramjet at mach 11[J].Journal of Propulsion and Power,2010,26(5):1125-1134
    [9]
    张静,阎超.高超音速双锥绕流数值模拟的格式效应分析[J].北京航空航天大学学报,2008,34(4):474-477 Zhang Jing,Yan Chao.Scheme effect of analysis of numerical simulation on hypersonic double-cone flows[J].Journal of Beijing University of Aeronautics and Astronautics,2008,34(4):474-477(in Chinese)
    [10]
    Michalak K,Olliver-Gooch C O.Limiters for unstructured higher-order accurate solutions of the Euler equations[R].AIAA Paper 2008-776,2008
    [11]
    Gnoffo P A.Updates to multi-dimensional flux reconstruction for hypersonic simulations on tetrahedral grids[R].AIAA Paper 2010-1271,2010
    [12]
    Gerlinger P.High-order multi-dimensional limiting for turbulent flows and combustion[R].AIAA Paper 2011-296,2011
    [13]
    李君哲,阎超,柯伦,等.气动热CFD计算的格式效应研究[J].北京航空航天大学学报,2003, 29(11):1022-1025 Li Junzhe,Yan Chao,Ke Lun,et al.Research on scheme effect of computational fluid dynamics in aerothermal[J].Journal of Beijing University of Aeronautics and Astronautics,2003, 29(11):1022-1025(in Chinese)
    [14]
    Hirsch C.Numerical computation of internal and external flows:volume 2 [M].New York: John Wiley & Sons Ltd,1990: 493-570
    [15]
    Miller C G.Experimental and predicted heating distributions for biconics at incidence in air at mach 10[R].NASA-TP-2334,1984
    [16]
    Olivier H,Gr nig H,Bozec A L.Hypersonic model testing in a shock tunnel [J].AIAA Journal,1995,33(2):262-265
    [17]
    Riedelbauch S,Brenner G,Muller B,et al.Numerical simulation of laminar hypersonic flow past a double-ellipsoid[R].AIAA Paper 89-1840,1989
    [18]
    李素循.典型外形高超声速流动特性[M].北京:国防工业出版社,2007:63-71 Li Suxun.Hypersonic characteristic of typical configuration[M].Beijing:National Defence Industry Press,2007:63-71(in Chinese)
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