| [1] | Luo Haibo, Zhang Daijun, Hui Bin, et al. Numerical calculation of turbulent convection heat transfer over infrared dome based on SST turbulence model[J]. Infrared and Laser Engineering, 2016, 45(7):0703002. (in Chinese) |
| [2] | Zhang Yiguang, Yang Jun, Li Xiaodan. Thermal property assessment experiment of the optic dome[J]. Infrared and Laser Engineering, 2008, 37(S):556-559. (in Chinese) |
| [3] | Crabtree L F, Dommentt R L, Woodley J G. Estimation of heat transfer to flat paltes, cones and blunt bodies[R]. Royal Aircraft Establishment Technical Report, No. 3637, 1965:1-25. |
| [4] | Menter F R, Langtry R, Vlker S, et al. Transition modelling for general purpose CFD codes[J]. Flow Turbulence and Combust, 2006, 77(1-4):227-303. |
| [5] | Stetson K F. Hypersonic boundary layer transition experiments[R]. AFWAL-TR-80-3062. Air Force Wright Aeronautical Laboratories, 1980. |
| [6] | Stetson K F. On predicting hypersonic boundary layer transition[R]. AFWAL-TM-87-160-FIMG. Air Force Wright Aeronautical Laboratories, 1987. |
| [7] | Stine H A, Wanlass K. Theoretical and experimental investigation of aerodynamic-heating and isothermal heat-transfer parameters on a hemispherical nose with laminar boundary layer at supersonic mach numbers[S]. NASA, NACA-TN-3344-1954. |
| [8] | Crawford D H, McCauley W D. Investigation of the laminar aerodynamic heat-transfer characteristics of a hemisphere-cylineder in the langley 11-inch hypersonic tunnel at a mach number of 6.8[R]. NASA, NACA TN 3706, 1956. |
| [9] | Beckwith I E, Gallagher J J. Heat transfer and recovery temperatures on sphere with laminar, transitional, and turbulenc t boundary layers at Mach number of 2.00 and 4.15[R]. NASA, NACA TN 4125, 1956. |
| [10] | Driest E R V. On the aerodynamic heating of blunt bodies[J]. ZAMP, 1958, 9(5-6):233-248. |
| [11] | Wu Zhen, Sun Luchao, Wang Jingyang. Effects of sintering method and sintering temperature on the microstructure and properties of porous Y2SiO5[J]. Journal of Materials Science Technology, 2015, 31(12):1237-1243. |
| [12] | Lili L V. Study of engineering method of calculation of aerodynamic heating of body at hypersonic[D]. Xi' an:Northwestern Polytech nical University, 2005:22-29. (in Chinese) |
| [13] | Aderson J D Jr. Hypersonic and High Temperature Gas Dynamic[M]. New York:McGraw-Hill, 1989:53-56, 152-155, 189-190, 286-288. |
| [14] | Li Fengwei, Song Wenping, Yang Yong, et al. Introduction to Aerodynamics[M]. Xi'an:Press of NWPU, 2007:181-189. (in Chinese) |
| [15] | Wang Xucheng. Finite Element Method[M]. Beijing:Tsinghua University Press, 2003:441-445. (in Chinese) |
| [16] | Bian Yingui, Xu Ligong. Aerothermodynamics[M]. Hefei:Press of University of Science and Technology of China, 2011:325-327. (in Chinese) |
| [17] | Klein C. Infrared missile domes:heat flux and thermal shock[C]//SPIE, 1993, 1997:150-169. |
| [18] | Yu Huaizhi. Infrared Optical Materials[M]. Beijing:National Defence Indurstry Press, 2007:126-127, 139-141. (in Chinese) |