Li Mao, Du Zhenggang, Jin Ping, et al. Numerical simulation of combustion for GH2/GO2 gas-fired shear coaxial injector[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(4): 469-473. (in Chinese)
Citation: Li Pengfei, Wu Songping. New interface boundary condition method for coupled thermal simulations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(9): 1071-1074. (in Chinese)

New interface boundary condition method for coupled thermal simulations

  • Received Date: 30 Apr 2010
  • Publish Date: 30 Sep 2010
  • A new interface boundary condition method was advanced for coupling between hypersonic flow field and structural heat transfer. The new coupling scheme consisted of solving an additional partial differential equation on the interface, which was derived from the Dirichlet and Neumann conditions at the interface. The interface solution was explicitly influenced by the two subdomains. The Godunov-Ryabenkii method was used to analyze the stability properties of the method. The analysis indicats that the method is not only more stable but also more accurate than the conventional method. The method proposed is applied for aerodynamically infinite column. The transformation of column-s temperature is detailedly analyzed during pneumatic heat.

     

  • [1] Giles M B.Stability analysis of numerical interface conditions in fluid-structure thermal analysis[J].International Journal of Numerical Methods in Fluids,1997,25(4):421-436 [2] Codina R,Houzeaux G.Numerical approximation of the heat transfer between domains separated by thinwalls[J].International Journal of Numerical Methods in Fluids,2006,52(9):963-986 [3] Felippa C A,Park K C.Staggered transient analysis procedures for coupled mechanical systems:formulaion[J].Computer Methods in Applied Mechanics and Engineering,1980,24:61-111 [4] Thornton E A,Dechaumphai P.Finite element prediction of aerothermal structural interaction of aerodynamically heated panels[R].AIAA87-1610,1987 [5] 夏刚,刘新建,程文科,等.钝体高超声速气动加热与结构热传递的耦合数值计算[J].国防科技大学学报,2003,25(1):35-39 Xia Gang,Liu Xinjian,Cheng Wenke,et al.Numerical simulation of fluid-solid-thermal interaction in hypersonic flows blunt aircraft[J].Journal of National University of Defense Technology,2003,25(1):35-39(in Chinese) [6] 黄春生,吴杰,范绪箕.飞行器流场与结构温度场耦合数值分析[J].力学与实践,2004,26(2):24-26 Huang Chunsheng,Wu Jie,Fan Xuji.Analysis of fluid-structure thermal simulations on the aircraft[J].Mechanics and Practice,2004,26(2):24-26(in Chinese) [7] Yoon S,Jameson A.Lower-upper symmetric Gauss-Sediel method for the Euler and Navier-Stokes equation[J].AIAA Journal,1988,26(9):35-39 [8] Yee H C,Kutler P. Application of second-order-accurate total variation diminishing(TVD)schemes to the euler equations in general geometries[R].NASA-TM-85845,1983 [9] Harten A. High Resolution schemes for hyperbolic conservation laws[J].Journal of Computational Physics,1983,49:357-393 [10] Roe B,Jaiman R,Haselbacher A,et al. Combined interface boundary condition method for coupled thermal simulations[J].International Journal for Numerical Methods in Fluids,2008,57(3):329-354 [11] Godunov S K,Ryabenkii V S.The theory of difference schemes:an introduction[M].North-holland,Amsterdam:North-Houand Pub Co,New York:Interscience Publishers,1964 [12] 谢锦睿.高超音速流动数值模拟与热流数值计算[D].北京航空航天大学航空科学与工程学院,2007 Xie Jinrui.Numerical simulation of hypersonic flows and calculation of aerothermal heating[D].School of Acronautic Science and Engineering,Beijing University of Aeronautics and Astronautiss,2007(in Chinese)
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