Tilmann C P, Bowersox R D W, Buter T A. On the design and construction of an academic Mach 5 wind tunnel, AIAA-1999-0800. Reston: AIAA, 1999.
[2]
Quan Z B, Xu J L, Li B, et al. Cold flow experiment and numerical study on nonuniform entrance of scramjet nozzle[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(10): 2308-2315. (in Chinese) 全志斌, 徐惊雷, 李斌, 等. 超燃冲压发动机尾喷管非均匀进口的冷流试验与数值模拟[J]. 航空学报, 2013, 34(10): 2308-2315.
[3]
Huang J, Liu G, Ma G F. Nonlinear optimal attitude tracking control of uncertain three-inline tethered satellite systems[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(4): 679-687. (in Chinese) 黄静, 刘刚, 马广富. 直连式三体绳系卫星姿态鲁棒最优跟踪控制[J]. 航空学报, 2012, 33(4): 679-687.
[4]
Young R H. Contra-rotating axial-flow fans[J]. Journal of Institute Heating Ventilating Engineering, 1951, 18: 448-477.
[5]
Sabel S, Sabatuik S. Turbojet engine development design of phase I & II compressor, Currtise Wright Cooperation(CWR), Report No. 502a and 502b. 1957.
[6]
Youssef N N. Radar cross section of complex targets [J]. Proceedings of the IEEE, 1989, 77(5): 722-734.
[7]
Millar D A J, Chappel M S, Okelah R. The co-turbo shaft-A novel gas turbine power plant for heavy equipment, ASME Paper, GT-79-132. New York: ASME, 1979.
[8]
Newton A G. Aero gas turbine engines for commercial application//7th International Symposium on Air Breathing Engines, 1985.
[9]
Baldeo M K. Unducted fan engines[J]. Boeing Airliner Magazine (USA), 1987(1-3): 1-15.
[10]
Schanzle A F. Horseshoe-shaped orbits in the Jupiter-Sun restricted problem[J]. The Astronomical Journal, 1967, 72(2): 149-157.
[11]
Wisler D C. Loss reduction in axial-flow compressor through low-speed model testing[J]. Journal of Engineering for Gas Turbines and Power, 1985, 107(2): 354-363.
[12]
Xu M, Xu S J. Stability analysis and transiting trajectory design for retrograde orbits around moon[J]. Journal of Astronautics, 2009, 30(5): 1785-1790. (in Chinese) 徐明, 徐世杰.绕月飞行的大幅值逆行轨道研究[J].宇航学报, 2009, 30(5): 1785-1790.
[13]
Yun Q L, Sun S P, Xu M F, et al. GJB 1179-91 Specification for flow field quality of high and low speed wind tunnels[S]. Mianyang: China Aerodynamics Research and Revelopment Center, 1991: 2-4. (in Chinese) 恽起麟, 孙绍鹏, 徐明方, 等. GJB1179-91 高速风洞低速风洞流场品质规范[S].绵阳: 中国空气动力研究与发展中心, 1991: 2-4.
[14]
Lai Y Y. Parameter optimization theory and explain examples in Isight[M]. Beijing: Beihang University Press, 2012: 66-79. (in Chinese) 赖宇阳. Isight参数优化理论与实例详解[M]. 北京: 北京航空航天大学出版社, 2012: 66-79.
[15]
Sharma P B, Adekoya A. A review of recent research on contra-rotating axial flow compressor stage, ASME Paper, GT-96-254. New York: ASME, 1996.
[16]
Zucrow M J, Hoffman J D. Gas dynamics-multidimensional flow[M]. New York: Wiley, 1977: 160-169.
[17]
Jin R, Chen W, Simpson T W. Comparative studies of metamodeling techniques under multiple modeling criteria [J]. Journal of Structural and Multidisciplinary Optimization, 2001, 23(1): 1-13.
[18]
Day I J. Stall inception in axial flow compressors[J]. Journal of Turbomachinery, 1993, 115(1): 1-9.
[19]
Qiu Y B. Experimental design and data processing[M]. Hefei: University of Science and Technology of China Press, 2008: 20-28. (in Chinese) 邱轶兵. 试验设计与数据处理[M]. 合肥: 中国科学技术大学出版社, 2008: 20-28.
