[1] 王勋年. 低速风洞试验[M]. 北京:国防工业出版社, 2002:135-145, 164-182. WANG X N. Low-speed wind tunnel testing[M]. Beijing:National Defense Industry Press, 2002:135-145, 164-182(in Chinese).
[2] 王发祥. 高速风洞试验[M]. 北京:国防工业出版社, 2001:155-170, 242-255. WANG F X. High-speed wind tunnel testing[M]. Beijing:National Defense Industry Press, 2001:155-170, 242-255(in Chinese).
[3] 吴子牛, 白晨媛, 李娟, 等. 高超声速飞行器流动特征分析[J]. 航空学报, 2015, 36(1):58-85. WU Z N, BAI C Y, LI J, et al. Analysis of flow characteristics for hypersonic vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1):58-85(in Chinese).
[4] GOON'KO Y P. Aerodynamic experimentation with ducted models as applied to hypersonic air-breathing vehicles[J]. Experiments in Fluids,1999,27(3):219-234.
[5] 余平, 段毅, 尘军. 高超声速飞行的若干气动问题[J]. 航空学报, 2015, 36(1):7-23. YU P, DUAN Y, CHEN J. Some aerodynamic issures in hypersonic flight[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1):7-23(in Chinese).
[6] 王泽江, 唐小伟, 宋文萍, 等. 圆截面超燃冲压发动机冷态内流测力试验[J]. 推进技术, 2016, 37(4):617-623. WANG Z J, TANG X W, SONG W P, et al. Zero-fuel internal flow force test for circular cross section scramjet engine[J]. Journal of Propulsion Technology, 2016, 37(4):617-623(in Chinese).
[7] 赵忠良, 杨晓娟, 蒋卫民, 等. 高超声速飞行器通流模拟方法与风洞验证技术[J]. 航空学报, 2014, 35(11):2932-2938. ZHAO Z L, YANG X J, JIANG W M, et al. Through-flow simulation method and wind tunnel validation technique for hypersonic vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(11):2932-2938(in Chinese).
[8] 许晓斌, 舒海峰, 谢飞, 等. 通气模型内流道阻力直接测量技术[J]. 推进技术, 2013, 34(3):311-315. XU X B, SHU H F, XIE F, et al. Technique investigation on flow through model inner flow drag straightway measured by strain-gauge balance[J]. Journal of Propulsion Technology, 2013, 34(3):311-315(in Chinese).
[9] 黄湛, 张江, 宫建, 等. DPIV技术在高超声速通气模型内阻测量中的应用[J]. 应用力学学报, 2014, 31(2):182-187. HUANG Z, ZHANG J, GONG J, et al. Application of internal drag DPIV measurement for hypersonic ducted models[J]. Journal of Applied Mechanics, 2014, 31(2):182-187(in Chinese).
[10] 唐志共, 许晓彬, 杨彦广, 等. 高超声速风洞气动力试验技术进展[J]. 航空学报, 2015, 36(1):86-97. TANG Z G, XU X B, YANG Y G, et al. Research progress on hypersonic wind tunnel aerodynamic testing techniques[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1):86-97(in Chinese).
[11] 张绍武, 关祥东, 朱涛, 等. 高超声速风洞进气道流量系数测量精度影响因素研究[J]. 推进技术, 2013, 34(4):470-476. ZHANG S W, GUAN X D, ZHU T, et al. Investigation on factors affecting the measurement accuracy for inlet flow coefficient in hypersonic wind tunnel[J]. Journal of Propulsion Technology, 2013, 34(4):470-476(in Chinese).
[12] 邓帆, 杜新, 谭慧俊, 等. 吸气式高超声速飞行器冷流试验设计及验证[J]. 北京航空航天大学学报, 2014, 40(10):1341-1348. DENG F, DU X, TAN H J, et al. Design and validation of cold-flow test for air-breathing hypersonic vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(10):1341-1348(in Chinese).
[13] KIRKHAM F S, CUBBAGE J M, VAHL W A, et al. Studies of airframe-propulsion-system integration for Mach 6 cruise vehicles:NASA TN D-4128[R].Washington, D.C.:NASA,1967.
[14] ELLISON J C. Investigation of the aerodynamic characteristics of a hypersonic transport model at Mach numbers to 6:NASA TN D-6191[R]. Washington, D.C.:NASA,1971.
[15] WIE D V, CORPENING G, MATTES L, et al. An experimental technique for the measurement of mass flow of scramjet inlets tested in hypersonic pulse facilities:AIAA-1989-2331[R]. Reston, VA:AIAA, 1989.
[16] 王刚, 杨彦广, 唐志共. 高超声速气动力试验模拟参数选择准则[J]. 航空学报, 2015, 36(3):789-796. WANG G, YANG Y G, TANG Z G. Criterion of selective simulation parameters for hypersonic aerodynamic test[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(3):789-796(in Chinese).
[17] 李国帅, 魏志, 李巍, 等. 现代试验设计方法在高速风洞试验中的应用[J]. 航空学报, 2015, 36(3):782-788. LI G S, WEI Z, LI W, et al. Using modern design of experiments methodologies for high speed wind tunnel tests[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(3):782-788(in Chinese).
[18] 唐志共. 高超声速气动力试验[M]. 北京:国防工业出版社, 2004:75-81, 198-202, 245-258. TANG Z G. Hypersonic aerodynamic test[M]. Beijing:National Defense Industry Press, 2004:75-81, 198-202, 245-258(in Chinese).
[19] 夏玉顺, 稀忠祥, 鲍国华. 风洞特种实验技术[M].西安:西北工业大学出版社, 1985:37-55. XIA Y S, XI Z X, BAO G H. Special wind tunnel experiment technology[M]. Xi'an:Northwestern Polytechnical University Press, 1985:37-55(in Chinese).
[20] 王泽江, 李绪国, 孙鹏, 等. 高超声速内外流解耦试验系统设计与验证[J]. 推进技术, 2015, 36(6):920-926. WANG Z J, LI X G, SUN P, et al. Design and verification for hypersonic external and internal decoupling test system[J]. Journal of Propulsion Technology, 2015, 36(6):920-926(in Chinese).
[21] 王泽江, 孙鹏, 李绪国, 等. 吸气式高超声速飞行器内外流同时测力试验[J]. 航空学报, 2015, 36(3):797-803. WANG Z J, SUN P, LI X G, et al. Force test on internal and external flow simultaneous measurement of air-breathing hypersonic vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(3):797-803(in Chinese). |