Yen J C,Wagner D A.Computational aeroacoustics using a simplified courant number insensitive CE/SE method .AIAA-2005-2820,2005
[2]
Van Leer B.Flux-vector splitting for the Euler equations[J].Lecture Notes in Physics ,1982,170: 507-512
[3]
Yoshihara H,Sacher P.Test cases for inviscid flow field methods .Advisory Group for Aerospace Research and Development (AGARD)-AR-211,1985
[4]
Roe P L.Approximate Riemann solvers,parameter vectors,and difference schemes[J].Journal of Computational Physics,1981,43(2): 357-372
[5]
Chang S C.The method of space-time conservation element and solution element—a new approach for solving the navier-stokes and euler equations[J].Journal of Computational Physics,1995,119(2): 295-324
[6]
Chang S C.Courant number insensitive CE/SE schemes .AIAA-2002-3890,2002
[7]
刘敏,吴克启.基于非结构网格CE/SE算法圆柱绕流气动声场模拟[J].工程热物理学报,2009(2):227-229 Liu Min,Wu Keqi.The aero-acoustics simulation of flow around a cylinder using unstructured CE/SE scheme[J].Journal of Engineering Thermophysics,2009(2):227-229(in Chinese)
[8]
凌文辉,赵书苗,刘建文,等.时空守恒CE/SE数值方法在凹槽燃烧流动中的应用研究[J].推进技术,2010(1):34-41 Ling Wenhui,Zhao Shumiao,Liu Jianwen,et al.Numerical investigations of the cavity combustion flow using the CE/SE method[J].Journal of Propulsion Technology,2010(1):34-41(in Chinese)
[9]
Ji Z,Zhou Y F.A comparison study of three CESE schemes in MHD simulation[J].Chinese Physics Letters,2010,27(8):085201
[10]
孙孔倩,樊未军,杨茂林.CE/SE 法模拟爆震波点火及传播过程[J].航空动力学报,2008,23(2): 244-250 Sun Kongqian,Fan Weijun,Yang Maolin.Numerical simulation of detonation ignition and propagation progress by CE/SE method[J].Journal of Aerospace Power,2008,23(2): 244-250(in Chinese)
[11]
崔树鑫,韩玉琪,高歌.二维翼型绕流的CE/SE方法[J].北京航空航天大学学报,2011,37(1): 21-24 Cui Shuxin,Han Yuqi,Gao Ge.Space-time conservation element and solution element method (CE/SE) applied to flows around 2D airfoil[J].Journal of Beijing University of Aeronautics and Astronautics,2011,37(1):21-24(in Chinese)
[12]
Zhang Z C,Yu S,Chang S C.A space-time conservation element and solution element method for solving the two-and three-dimensional unsteady Euler equations using quadrilateral and hexahedral meshes[J].Journal of Computational Physics,2002,175(1):168-199
[13]
Yen J C,Wagner D A.Computational aeroacoustics using a simplified courant number insensitive CE/SE method .AIAA-2005-2820,2005
[14]
Yoshihara H,Sacher P.Test cases for inviscid flow field methods .Advisory Group for Aerospace Research and Development (AGARD)-AR-211,1985
