整流罩层流换热瞬时温升计算及其结构改进
[1] 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, V 觟lker 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 turbulenct 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 Polytechnical 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)
张代军, 罗海波, 常铮, 惠斌. 整流罩层流换热瞬时温升计算及其结构改进[J]. 红外与激光工程, 2018, 47(2): 0204004. Zhang Daijun, Luo Haibo, Chang Zheng, Hui Bin. Calculation of transient temperature rise of dome under laminar heat transfer condition and improvement of dome structure[J]. Infrared and Laser Engineering, 2018, 47(2): 0204004.