| [1] Oswatisch K. Pressure recovery in missiles with reaction propulsion at high supersonic speeds, NASA-TM-1140. Washington, D.C.: NASA, 1947.[2] Mlder S, Spiro E J. Busemann inlet for hypersonic speeds[J]. Journal of Spacecraft and Rockets, 2006, 3(8): 1303-1304.[3] van Wie D M, Mlder S. Applications of Busemann inlet designs for flight at hypersonic speeds, AlAA-1992-1210. Reston: AIAA, 1992.[4] Billig F S, Kothari A P. Streamline tracing: technique for designing hypersonic vehicles[J]. Journal of Propulsion and Power, 2000, 16(3): 465-471.[5] O'Brien T F. Viscous-optimized length-constrained axisymmetric geometries for streamline-tracing, AIAA-2008-2511. Reston: AIAA, 2008.[6] Nan X J, Zhang K Y, Jin Z G, et al. Investigation on hypersonic inward turning inlets with controlled pressure gradient[J]. Journal of Aerospace Power, 2011, 26(3): 518-523. (in Chinese) 南向军, 张堃元, 金志光, 等. 压升规律可控的高超声速内收缩进气道设计[J]. 航空动力学报, 2011, 26(3): 518-523.[7] Li Y Z, Zhang K Y, Nan X J. Design of hypersonic inward turning inlets base on concept controllable Mach number distribution[J]. Journal of Aerospace Power, 2012, 27(11): 2484-2491. (in Chinese) 李永洲, 张堃元, 南向军. 基于马赫数分布规律可控概念的高超声速内收缩进气道设计[J]. 航空动力学报, 2012, 27(11): 2484-2491.[8] He X Z, Zhou Z, Ni H L. Integrated design method and performance analyses of osculating inward turning cone waverider forebody inlet[J]. Journal of Propulsion and Technology, 2012, 33(4): 510-515. (in Chinese) 贺旭照, 周正, 倪鸿礼. 密切内锥乘波前体进气道一体化设计和性能分析[J]. 推进技术, 2012, 33(4): 510-515.[9] He X Z, Ni H L. Osculating curved cone (OCC) waverider: design methods and performance analysis[J]. Chinese Journal of Theoretical and Applied Mechanics, 2011, 43(6): 1077-1082. (in Chinese) 贺旭照, 倪鸿礼. 密切曲面锥乘波体-设计方法与性能分析[J]. 力学学报, 2011, 43(6): 1077-1082.[10] You Y C, Liang D W. Three-dimensional sections hypersonic inlet based on internal waverider[J]. Sci China Ser E-Tech Sci, 2009, 39(8): 1483-1494. (in Chinese) 尤延铖, 梁德旺. 基于内乘波概念的三维变截面高超声速进气道[J]. 中国科学 E辑: 技术科学, 2009, 39(8): 1483-1494.[11] Xiao Y B, Yue L J, Gong P, et al. Investigation on a truncated streamline-traced hypersonic Busemann inlet, AIAA-2008-2634. Reston: AIAA, 2008.[12] Sobieczky H, Dougherty F C, Jones K. Hypersonic waverider design from given shock waves//First International Waverider Symposium. College Park: University of Maryland, 1990: 17-19.[13] Eggers T, Sobieczky H, Center K B. Design of advanced waveriders with high aerodynamic efficiency, AIAA-1993-5141. Reston: AIAA, 1993.[14] Sobieczky H, Zores B, Wang Z, et al. High flow speed design using the theory of oculating cones and axisymmetric flows[J]. Chinese Journal of Aeronautics, 1999, 12(1): 1-7.[15] Zucrow M J, Hoffman J D. Gas dynamics[M]. New Yorks: John Wiley & Sons, Inc., 1976: 191-192.[16] Zhu X X. Plastic arts of free curves and curved surfaces[M]. Beijing: Science Press, 2000: 118-121. (in Chinese) 朱心雄. 自由曲线曲面造型技术[M]. 北京: 科学出版社, 2000: 118-121. |
CJA
