[1] K Pietrykowski, P Karpiński, R Mczka. Computational fluid dynamics model of various types of rocket engine nozzles. International Review on Modelling and Simulations, 13, 1-7(2020).

[2] X M Yin, L Wang, X L Zhang, et al. Wide band k-distribution model for calculating radiation signal of liquid rocket exhaust plume. Laser & Infrared, 50, 1352-1357(2020).

[3] J K Qi, S K Dong. Research on radiation characteristics of typical hypersonic targets. Tactical Missile Technology, 17-28(2021).

[4] Y Rivera, J L Muoz-Cobo, C Berna, et al. CFD simulation plus uncertainty quantification of the mixing of two fluid with different density for the Cold-Leg mixing benchmark. Nuclear Engineering and Design, 383, 111449(2021).

[5] L Li. Investigation of CFD uncertainty quantification approaches towards aeronautical applications. Aeronautical Science & Technology, 33, 46-56(2022).

[6] L Xia, S Yuan, Z J Zou, et al. Uncertainty quantification of hydrodynamic forces on the DTC model in shallow water waves using CFD and non-intrusive polynomial chaos method. Ocean Engineering, 198, 106920(2020).

[7] C W Jiang, X Liu, E Shi, et al. Uncertainty quantification of flow and heat transfer problems with stochastic boundary conditions based on the intrusive polynomial chaos expansion method. Applied Mathematics and Mechanics, 42, 481-491(2021).

[8] P B Du, Y Liu, Z H Chen, et al. Uncertainty quantification for turbulence effect of laser propagation in atmosphere based on polynomial chaos. Modern Applied Physics, 12, 31-36(2021).

[9] Y Q Sun, S K Dong, Q L Niu, et al. NIPC-based uncertainty analysis of infrared radiation from rocket exhaust plumes caused by nozzle exit conditions. Infrared Physics & Technology, 108, 103376(2020).

[10] [10] Dai W. Surrogate model of high temper ature plume radiation identification of engine parameters[D]. Harbin: Harbin Institute of Technology, 2021. （in Chinese)

[11] [11] Wang W C, Wei Z J, Zhang Q, et al. Study on infrared signature of solid rocket mot afterburning exhaust plume[C]46th AIAAASMESAEASEE Joint Propulsion Conference & Exhibit, 2010.

[12] [12] Ludwig C B, Malkmus W, Reardon J, et al. Hbook of infrared radiation from combustion gases[R]. NASASP3080, 1973.

[13] F F Xiong, J T Chen, C K Ren, et al. Recent advances in polynomial chaos method for uncertainty propagation. Chinese Journal of Ship Research, 16, 19-36(2021).

[14] Q L Niu, Z H He, S K Dong. IR radiation characteristics of rocket exhaust plumes under varying motor operating conditions. Chinese Journal of Aeronautics, 30, 1101-1114(2017).

[15] [15] Brentner K, Gimelshein S, Levin D, et al. Investigation of soot combustion in underexped jet plume flows[C]Proceedings of the 41st Aerospace Sciences Meeting Exhibit, 2003.

[16] K Viswanath, K S Brentner, S F Gimelshein, et al. Investigation of soot combustion in underexpanded jet plume flows. Journal of Thermophysics & Heat Transfer, 19, 282-293(2005).

[17] [17] Plastinin Y, Karabadzhak G, Khmelinin B, et al. Modeling of OH ultraviolet radiation in Atlas mot plume comparison with recent experimental data[C]41st Aerospace Sciences Meeting Exhibit, 2003.

[18] A A Alexeenko, N E Gimelshein, D A Levin, et al. Modeling of flow and radiation in the Atlas plume. Journal of Thermophysics and Heat Transfer, 16, 50-57(2002).

[19] [19] Alexeenko A A, Gimelshein N E, Levin D A, et al. Modeling of radiation in Atlas plumeflow[C]39th Aerospace Sciences Meeting & Exhibit, 2001.

[20] [20] Wang C L. Significance analysis of thrusters based on dynamic positioning capability of vessels[D]. Tianjin: Tianjin University of Technology, 2020. (in Chinese)