[1] YOON S, JAMESON A. Lower-upper symmetric-Gauss-Sediel method for the Euler and Navier-Stoker equations[J]. AIAA Journal, 1988, 26(9):1025-1026.
[2] KANDULA M, BUNING P G. Implementation of LU-SGS algorithm and Roe upwinding scheme in OVERFLOW thin-layer Navier-Stokes code:AIAA-1994-2357[R]. Reston:AIAA, 1994.
[3] CHEN K H, DUNCAN B, FRICKER D, et al. ALLSPD-3D[CP]. Washington, D. C.:NASA Lewis Research Center, 1996.
[4] KIM S L, JEUNG I S, PARK Y H, et al. Approximate Jacobian methods for efficient calculation of reactive flows:AIAA-2000-3384[R]. Reston:AIAA, 2000.
[5] EBERHARDT S, IMLAY S. Diagonal implicit scheme for computing flows with finite rate chemistry[J]. Journal of Thermophysics and Heat Transfer, 1992, 6(2):208-216.
[6] JU Y. Lower-upper scheme for chemically reacting flow with finite rate chemistry[J]. AIAA Journal, 1995, 33(8):1418-1425.
[7] CHIANG T L, HOFFMANN K. Determination of computational time step for chemically reacting clows:AIAA-1989-1855[R]. Reston:AIAA, 1989.
[8] KIM S L, CHOI J Y, JEUNG I S, et al. Application of approximate chemical Jacobians for constant volume reaction and shock-induced combustion[J]. Applied Numerical Mathematics, 2001, 39:87-104.
[9] ANDERSON D A, TANNEHILL J C, PLETCHER R H. Computational fluid mechanics and heat transfer[M]. 3rd ed. New York:Hemisphere Publishing Corporation, 1994:82-89.
[10] 瞿章华. 高超声速空气动力学[M]. 长沙:国防科技大学出版社, 2001:182-186. QU Z H. Hypersonic aerodynamics[M]. Changsha:National University of Defence Technology Press, 2001:182-186(in Chinese).
[11] DUNN M G, KANG S W. Theoretical and experimental studies of reentry plasmas:NASA CR-2232[R]. Washington, D. C.:NASA, 1973.
[12] 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, 2006:148-151. YAN C. The method and application for computatinal fluid dynamics[M]. Beijing:Beihang University Press, 2006:148-151(in Chinese).
[13] BEAM R M, WARMING R F. An implicit finite difference algorithm for hyperbolic system in conservation law form[J]. Journal of Computational Physics, 1976, 22:87-109.
[14] ROE P L. Approximate riemann solvers, parameter vectors and difference schemes[J]. Journal of Computational Physics, 1981, 43:357-372.
[15] 蔡晋生, 李凤蔚, 罗时钧. 跨声速大迎角Euler方程数值分析[J]. 航空学报, 1993, 14(5):235-240. CAI J S, LI F W, LUO S J. A numerical solution of transonic Euler equation at high angles of attack[J]. Acta Aeronautica et Astronautica Sinica, 1993, 14(5):235-240(in Chinese).
[16] RICHARD P D. Efficiency improvements of RANS-based analysis and optimization using implicit and adjoint methods on unstructured grids[D]. Manchester:University of Manchester, 2006:63-73.
[17] ANDERSON J D. Hypersonic and high temperature gas dynamics[M]. New York:McGraw-Hill Book Company, 1989:476-477.
[18] BUSSING T R, MURMAN E M. Finite volume method for the calculation of compressible chemically reacting flows[J]. AIAA Journal, 1988, 26(9):1070-1078.
[19] HASSAN B, CANDLER G V, OLYNICK D R. Thermo-chemical nonequilibrium effects on the aerothermodynamics of aerobraking vehicles[J]. Journal of Spacecraft and Rockets, 1993, 30(6):647-655.
[20] 李海燕. 高超声速高温气体流场的数值模拟[D]. 绵阳:中国空气动力研究与发展中心, 2007:63-64. LI H Y. Numerical simulation of hypersonic and high temperature gas flowfield[D]. Mianyang:China Aerodynamics Research and Development Center, 2007:63-64(in Chinese).
[21] 潘沙. 高超声速气动热数值模拟方法及大规模并行计算研究[D]. 长沙:国防科学技术大学, 2010:143. PAN S. Hypersonic aerothermal numerical simulation method and massive parallel computation research[D]. Changsha:National University of Defense Technology, 2010:143(in Chinese).
[22] MUYLAERT J, WALPOT L, HAUSER J, et al. Standard model testing in the European high enthalpy facility F4 and extrapolation to flight:AIAA-1992-3905[R]. Reston:AIAA, 1992. |