[1] SCALABRIN L C,BOYD I D.Numerical simulation of weakly ionized hypersonic flow for reentry configurations:AIAA-2006-3773[R].Reston:AIAA,2006.
[2] PANDOLFI M,ARINA R,BOTTA N.Nonequilibrium hypersonic flows over corners[J].AIAA Journal,1991,29(2):235-241.
[3] FREDERICKSON K,LEONOV S,NISHIHARA M,et al.Energy conversion in high enthalpy flows and non-equilibrium plasmas[J].Progress in Aerospace Sciences,2015,72:49-65.
[4] AIT-ALI-YAHIA D,HABASHI W G.Finite element adaptive method for hypersonic thermochemical nonequilibrium flows[J].AIAA Journal,1997,35(8):1294-1302.
[5] YUMUSAK M,EYI S.Aerothermodynamic shape optimization of hypersonic blunt bodies:AIAA-2013-2693[R].Reston:AIAA,2013.
[6] BHUTTA B A,LEWIS C H.Three-dimensional hypersonic nonequilibrium flows at large angles of attack[J].Journal of Spacecraft and Rockets,1989,26(3):158-166.
[7] ZOBY E V,LEE K P,GUPTA R N,et al.Viscous shock-layer solutions with nonequilibrium chemistry for hypersonic flows past slender bodies[J].Journal of Spacecraft and Rockets,1989,26(4):221-228.
[8] PEZZELLA G,VOTTA R.Finite rate of chemistry effects on the high altitude aerodynamics of an Apollo-shaped reentry capsule:AIAA-2009-7306[R].Reston:AIAA,2009.
[9] 柳军,刘伟,曾明,等.高超声速三维化学非平衡流场的数值模拟[J].力学学报,2003,35(6):730-734.LIU J,LIU W,ZENG M,et al.Numerical simulation of 3D hypersonic thermochemical nonequilibrium flow[J].Acta Mechanica Sinica,2003,35(6):730-734(in Chinese).
[10] 董维中,丁明松,高铁锁,等.热化学非平衡模型和表面温度对气动热计算影响分析[J].空气动力学学报,2013,31(6):692-698.DONG W Z,DING M S,GAO T S,et al.The influence of thermo-chemical non-equilibrium model and surface temperature on heat transfer rate[J].Acta Aerodynamica Sinica,2013,31(6):692-698(in Chinese).
[11] 李康,胡宗民,姜宗林.热化学非平衡流动中粘性干扰和化学反应对HB2气动力的影响[J].中国科学:物理学,力学和天文学,2015,45(4):044702.LI K,HU Z M,JIANG Z L.Effect of viscosity and chemical reactions on aerodynamic force in chemical nonequilibrium flow[J].Scientia Sinica:Physica,Mechanica & Astronomica,2015,45(4):044702(in Chinese).
[12] 周禹,阎超.高超声速热化学非平衡空间格式的扩展与改进[J].北京航空航天大学学报,2010,36(2):193-197.ZHOU Y,YAN C.Extension and improvement for schemes in hypersonic thermal and chemical non-equilibrium flows[J]. Journal of Beijing University of Aeronautics and Astronautics,2010,36(2):193-197(in Chinese).
[13] 周印佳,孟松鹤,解维华,等.高超声速飞行器热环境与结构传热的多场耦合数值研究[J].航空学报,2016,37(9):2739-2748.ZHOU Y J,MENG S H,XIE W H,et al.Multi-field coupling numerical analysis of aerothermal environment and structural heat transfer of hypersonic vehicles[J].Acta Aeronautica et Astronautica Sinica,2016,37(9):2739-2748(in Chinese).
[14] FORD D I,JOHNSON R E.Dependence of rate rate constants on vibrational temperatures:An arrhenius description:AIAA-1988-0461[R].Reston:AIAA,1988.
[15] GUPTA R N,YOS J M,THOMPSON R A,et al.A review of reaction rates and thermodynamic and transport properties for an 11-species air model for chemical and thermal nonequilibrium calculations to 30000K:NASA RP-1232[R].Washington,D.C.:NASA,1990.
[16] PARK C.On convergence of computation of chemical reacting flows:AIAA-1985-0247[R].Reston:AIAA,1985.
[17] PARK C.Problems of rate chemistry in the flight regimes of aeroassisted orbital transfer vehicles:AIAA-1984-1730[R].Reston:AIAA,1984.
[18] CANDLER G V,MACCORMACK R W.The computation of hypersonic ionized flows in chemical and thermal nonequilibrium:AIAA-1988-0511[R].Reston:AIAA,1988.
[19] WILKE C R.A viscosity equation for gas mixtures[J].Journal of Chemical Physics,1950,18(4):517-519.
[20] YOON B,RASMUSSEN M L.Diffusion effects in hypersonic flows with a ternary mixture[J].KSME International Journal,1999,13(5):432-442.
[21] MACLEAN M,MARINEAU E,PARKER R,et al.Effect of surface catalysis on measured heat transfer in expansion tunnel facility[J].Journal of Spacecraft and Rockets,2013,50(2):470-474.
[22] HORNUNG H G,WEN C Y.Nonequilibrium dissociationg flow over spheres:AIAA-1995-0091[R].Reston:AIAA,1995.
[23] STEWART D A,CHEN Y K.Hypersonic convective heat transfer over 140-deg blunt cones in different gases[J].Journal of Spacecraft and Rockets,1994,31(5):735-743. |