[1] [1] Rankin B A, Ihme M, Gore J. Quantitative model-based imaging of mid-infrared radiation from a turbulent non-premixed jet flame and plume［J］. Combustion and Flame, 2015, 162(4): 1275-1283.

[2] [2] Blunck D, Harvazinski M, Rankin R, et al. Turbulent radiation statistics of exhaust plumes exiting from a subsonic axisymmetric nozzle［J］. Journal of Thermophysics and Heat Transfer, 2012, 26(2): 286-293.

[3] [3] Blunck D L, Harvazinksi M E, Merkle C L, et al. Influence of turbulent fluctuations on the radiation intensity emitted from exhaust plumes［J］. Journal of Thermophysics and Heat Transfer, 2012, 26(4): 581-589.

[4] [4] Blunck D L, Gore J. Study of narrowband radiation intensity measurements from subsonic exhaust plumes［J］. Journal of Propulsion and Power, 2011, 27(1): 227-235.

[5] [5] Mahulikar S P, Potnuru S K, Rao G A. Study of sunshine, skyshine, and earthshine for aircraft infrared detection［J］. Journal of Optics A, 2009, 11(4): 045703.

[6] [6] Liu Zunyang, Shao Li, Wang Yafu, et al. Influence of flight parameters on the infrared radiation of a liquid rocket exhaust plume［J］. Acta Optica Sinica, 2013, 33(4): 0404001.

[7] [7] Liu Zunyang, Shao Li, Wang Yafu, et al. Influence of afterburning on the infrared radiation of solid rocket exhaust plume［J］. Acta Optica Sinica, 2013, 33(6): 0604001.

[8] [8] Liu Zunyang, Shao Li, Wang Yafu, et al. Influence of afterburning on infrared radiation of liquid rocket exhaust plume［J］. Acta Photonica Sinica, 2013, 42(4): 480-485.

[9] [9] Wang Weichen, Li Shipeng, Zhang Qiao, et al. Influence of operating conditions on temperature distributions of exhaust plume of solid rocket motor［J］. Acta Armamentarii, 2011, 32(12):1493-1498.

[10] [10] Fiveland W A, Jamaluddin A S. Three-dimensional spectral radiative heat transfer solutions by the discrete-ordinates method［J］. Journal of Thermophysics and Heat Transfer, 1991, 5(3):335-339.

[11] [11] Alberti M, Weber R, Mancini M, et al. Comparison of models for predicting band emissivity of carbon dioxide and water vapour at high temperatures［J］. International Journal of Heat and Mass Transfer, 2013, 64: 910-925.

[12] [12] Rothman L S, Gordon I Z, Barber R J, et al. HITEMP, the high-temperature molecular spectroscopic database［J］. Journal of Quantitative Spectroscopy & Radiative Transfer, 2010, 111(15): 2139-2150.

[13] [13] Alberti M, Weber R, Mancini M, et al. Validation of HITEMP-2010 for carbon dioxide and water vapor at high temperatures and atmospheric pressures in 450-7600 cm-1 spectral range［J］. Journal of Quantitative Spectroscopy and Radiative Transfer, 2015, 157: 14-33.

[14] [14] Laraia A L, Gamache R R, Lamouroux J, et al. Total internal partition sums to support planetary remote sensing［J］. Icarus, 2011, 215(1): 391-400.

[15] [15] Clough S A, Shephard M W, Mlawer E J, et al. Atmospheric radiative transfer modeling: A summary of the AER codes［J］. Journal of Quantitative Spectroscopy & Radiative Transfer, 2005, 91(2): 233-244.

[16] [16] Coppalle A, Vervisch P. The total emissivities of high-temperature flames［J］. Combustion and Flame, 1983, 49(1/2/3): 101-108.

[17] [17] Edwards D K, Matavosian R. Scaling rules for total absorptivity and emissivity of gases［J］. Journal of Heat Transfer, 1984, 106(4): 684-689.

[18] [18] Molvik G, Merkle C. A set of strongly coupled, upwind algorithms for computing flows in chemical non-equilibrium［C］. 27th Aerospace Sciences Meeting and Exhibit, 1989: 199.

[19] [19] Sinha N, Dash S, Hosangadi A. Applications of an implicit, to steady/unsteady reacting, upwind Navier-Stokes code, CRAFT, multi-phase flowfields［C］. 30th Aerospace Sciences Meeting and Exhibit, 1992: 837.

[20] [20] York B, Sinha N, Dash S. Navier-Stokes simulation of plume vertical launching system interaction flowfields［C］. 30th Aerospace Sciences Meeting and Exhibit, 1992: 839.

[21] [21] Rao R, Candler G, Wright M. Numerical simulations of Atlas II rocket motor plumes［C］. 35th Joint Propulsion Conference and Exhibit, 1999: 2258.

[22] [22] Candler G, Rao R, Sinha K. Numerical simulations of Atlas-II rocket motor plumes［C］. 39th Aerospace Sciences Meeting and Exhibit, 2001: 354.

[23] [23] Jachimowski C J. An analytical study of the hydrogen-air reaction mechanism with application to scramjet combustion［R］. NASA Langley Research Center, 1988: 2791.

[24] [24] Cocks P, Dawes W, Cant R. The influence of turbulence-chemistry interaction modelling for supersonic combustion［C］. 49th Aerospace Sciences Meeting and Exhibit, 2011: 306.

[25] [25] Roblin A, Dubois I, Grisch F. Comparison between computations and measurements of a H2/LOX rocket motor plume［C］. 8th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, 2002: 3107.

[26] [26] Calhoon W H, Kenzakowsk D C. Flowfield and radiation analysis of missile exhaust plumes using a turbulent-chemistry interaction model［C］. 36th Joint Propulsion Conference and Exhibit, 2000: 3388.

[27] [27] Calhoon W H. Computational assessment of afterburning cessation mechanisms in fuel-rich rocket exhaust plumes［J］. Journal of Propulsion and Power, 2001, 17(1): 111-119.

[28] [28] Calhoon W H, Kenzakowsk D C. Assessment of turbulence -chemistry interactions in missile exhaust plume signature analysis［J］. Journal of Spacecraft and Rockets, 2003, 40(5): 694-695.

[29] [29] Calhoon W, Brinckman K, Tomes J, et al. Scalar fluctuation and transport modeling for application to high speed reacting flows［C］. 44th Aerospace Sciences Meeting and Exhibit, 2006: 1452.

[30] [30] Devir A, Lessin A, Lev M, et al. Comparison of calculated and measured radiation from a rocket motor plume［C］. 49th Aerospace Sciences Meeting and Exhibit, 2011: 358.