[1] Walker S H, Sherk J, Shell D, et al. The DARPA/AF falcon program: the hypersonic technology vehicle# 2(HTV-2) flight demonstration phase[C]//15th AIAA International Space Planes and Hypersonic System and Technologies Conference, 2008.
[2] Blanchard R, Anderson B, Welch S, et al. Shuttle orbiter fuselage global yemperature measurements from infrared images at hypersonic speeds[C]//Atmospheric Flight Mechanics Confernce and Exhibit, 2013, 19(55): 153-170.
[3] Mahulkar S P, Songawane H R, Rao G A. Infrared signature studies of aerospace vehicles[J]. Progress in Aerospace Sciences, 2007, 43(7): 218-245.
[4] Ross M, Werner M, Mazuk S, et al. Infrared imagery of the space shuttle at hypersonic entry conditions[C]//46th AIAA Aerospace Sciences Meeting and Exhibit, 2008(1): 7-10.
[5] Horvath, Thomas J. Remote observations of reentering spacecraft including the space shuttle orbiter[C]//IEEE Aerospace Conference, 2013: 6497380.
[6] Schwartz R, Verstynen H, Gruber J, et al. Remote infrared imaging of the space shuttle during hypersonic flight: HYTHIRM mission operations and coordination[C]//42nd AIAA Thermophysics Conference, 2011: 27-30.
[7] Brandis A M, Johnston C O, Cruden B A, et al. Uncertainty analysis and validation of radiation measurements for earth reentry[J]. Journal of Thermophysics and Heat Transfer, 2015, 29(2): 209-221.
[8] Ozawa T, Garrison M B, Levin D A. Accurate molecular and soot infrared radiation model for high-temperature flows[J]. Journal of Thermophysics and Heat Transfer, 2007, 21(1): 19-27.
[9] Andrienko D A, Boyd I D. Kinetic models of oxygen thermochemistry based on quasi-classical trajectory analysis[J]. Journal of Thermophysics and Heat Transfer, 2016, 30(1): T4968.
[10] Park C. Assessment of two-temperature kinetic model for ionizing air[J]. Journal of Thermophysics and Heat Transfer, 1989, 3(3): 233-244.
[11] Perrin M Y, Colonna G, D′Ammando G, et al. Radiation models and radiation transfer in hypersonics[J]. The Open Plasma Physics Journal, 2014, 7(1): 114-126.
[12] Gnoffo P A. Upwind-biased, point-implicit relaxation strategies for viscous, hypersonic flows[C]//9th Computational Fluid Dynamics Conference, 1989(6): 13-15.
[13] Shao C, Nie L, Chen W. Analysis of weakly ionized ablation plasma flows for a hypersonic vehicle[J]. Aerospace Science and Technology, 2016, 51: 151-161.
[14] Menter F R, Kunta M, Langtry R. Ten years of industrial experience with the SST turbulence model[J]. Heat and Mass Transfer, 2003, 4(1): 625-632.
[15] Surahikov S. Radiative gas dynamics of MSL at angle of attack[C]//54th AIAA Aerospace Sciences Meeting, 2016(1): 4-8.
[16] Willams F A. Combustion Theory[M]. 2nd ed. US: Benjamin/Cummings, Inc., 1985.
[17] Liu Y, Vinpkur M. Upwind algorithms for nonequilibrium flows[C]//27th AIAA Aerospace Sciences Meeting, 1989(1): 9-12.
[18] Nam H J, Kwon O J. Infrared radiation modeling of NO, OH, CO, H2O, and CO2 for emissivity/radiance prediction at high temperature[J]. Infrared Physics & Technology, 2014, (8): 001-003.
[19] Mu L, Ma Y, He Z, et al. Radiation characteristics simulation of non-equilibrium flow field around the hypersonic blunted cone[J]. Journal of Engineering Thermophysics, 2012, 33(11): 1958-1962.
[20] Rothman L, Gordon I, Barber R, et al. HITEMP, the high-temperature molecular spectroscopic database[J]. Journal of Quantitative Spectroscopy and Radiative Transfer, 2010, 111(15): 2139-2150.
[21] Niu Q, He Z, Dong S. Prediction of shock-layer ultraviolet radiation for hypersonic vehicles in near space[J]. Chinese Journal of Aeronautics, 2016, 29(5): 1367-1377.
[22] Ren K, Tian J, Gu G, et al. Operating distance calculation of ground-based and air-based infrared system based on Lowtran7[J]. Infrared Physics & Technology, 2016, 77(7): 414-420.
[23] Ferrero P, D′Ambrosio D. A numerical method for conjugate heat transfer problems in hypersonic flows[C]//40th Thermophysics Conference, 2008(6): 4247.
[24] Packan D, Laux C O, Gessman R J, et al. Measurement and modeling of OH, NO, and CO infrared radiation at 3 400 K[J]. Journal of Thermophysics and Heat Transfer, 2003, 17(4): 450-456.
[25] Zhen Huaping, Jiang Chongwen. Review on hypersonic technology verification HTV-2 vehicle[J]. Winged Missile Journal, 2013, 6(6): 7-13. (in Chinese)
[26] Cheng H K. Perspectives on hypersonic viscous and nonequilibrium flow research[R]. NASA-CR-190817, 1992: 140151.
[27] Acton J M. Hypersonic boost-glide weapons[J]. Science & Global Security, 2015, 23(3): 191-192.
