| Citation: | WANG Chao, WU Song-ping. Improved weighted essential non-oscillatory methods in hypersonic heat-flux simulation[J]. Journal of Aerospace Power, 2012, 27(11): 2499-2504.
|
| [1] |
Harten A.High resolution schemes for hyperbolic systems of conservation laws[J].Journal of Computational Physics,1983,49(3):357-393.
|
| [2] |
Jameson A,Lax P D.Condition for the construction of multi-point total variation diminishing difference schemes.ICASE Reprot 86-18,1986.
|
| [3] |
Yee H C.Upwind and symmetric shock capturing schemes.NASA TM 89464,1987.
|
| [4] |
Roe P L.Approximate Riemann solvers,parameter vectors,and different schemes[J].Journal of Computational Physics,1981,43(2):357-372.
|
| [5] |
Harten A,Engquist B,Osher S,et al.Uniformly high order accurate essentially non-oscillatory schemes[J].Journal of Computational Physics,1989,71(2):231-303.
|
| [6] |
Liu X D,Osher S,Chan T.Weighted essentially non-oscillatory schemes[J].Journal of Computational Physics,1994,115(1):200-212.
|
| [7] |
Jiang X D,Shu C W.Efficient implementation of weighted ENO schemes[J].Journal of Computational Physics,1996,126(1):202-228.
|
| [8] |
Titarev V A,Toro E F.Finite-volume WENO schemes for three-dimensional conservation laws [J].Journal of Computational Physics,2004,201(1):138-260.
|
| [9] |
Zhou T,Li Y,Shu C W.Numerical comparison of WENO finite volume and runge-kutta discontinuous galerkin methods[J].Journal of Scientific Computing,2001,16(2):145-171.
|
| [10] |
Wolf W R,Joao L F.Azevedo.Supersonic and hypersonic flow computations using high-order non-oscillatory schemes [J].AIAA-2006-3169,2006.
|
| [11] |
Rehman S F,Eldredge J D,ZHONG Xiaolin.An evaluation of shock-capturing methods on a hypersonic boundary layer receptivity problem [R].AIAA-2009-941,2009.
|
| [12] |
Lee J,Huerta M A,ZHA Gecheng.Hypersonic 3-D blunt body equilibrium air flow using high order WENO schemes [R].AIAA-2010-4765,2010.
|
| [13] |
SHEN Yiqing,ZHA Gecheng,Huerta M A.Simulation of hypersonic wave/boundary layer interaction using high order WENO scheme [R].AIAA-2010-1047,2010.
|
| [14] |
Cleary J W.Effects of angle of attack and bluntness on laminar heating-rate distributions of a 15° cone at a Mach number of 10.6 [R].NASA TN D-5450,1969.
|
| [15] |
Miller C G.Experimental and predicted heating distributions for biconics at incidence in air at Mach 10 [R].NASA-TP-2334,1984.
|
DownLoad: