[1] 卫锋, 贺旭照, 贺元元, 等. 三维内转式进气道双激波基准流场的设计方法[J]. 推进技术, 2015, 36(3): 358-364. (WEI Feng, HE Xu-zhao, HE Yuan-yuan, et al. Design Method of Dual-Shock Wave Basic Flow-Field for Inward Turning Inlet[J]. Journal of Propulsion Technology, 2015, 36(3): 358-364.)
[2] Sobieczky H, Dougherty F C, Jones K. Hypersonic Waverider Design from Given Shock Wave[C]. College Park: University of Maryland: First International Waverider Symposium, 1990.
[3] Eggers T, Sobieczky H, Center K B. Design of Advanced Waveriders with High Aerodynamic Efficiency[R]. AIAA 93-5141.
[4] 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.
[5] 高文智, 李祝飞, 杨基明, 等. 一种用于前缘钝化高超声速进气道设计评估的CFD/特征线组合方法及其应用[J]. 推进技术, 2013, 34(12): 1585-1592. (GAO Wen-zhi, LI Zhu-fei, YANG Ji-ming, et al. A Combined CFD/Characteristic Method for Design and Performance Prediction of Hypersonic Inlet with Leading Edge Bluntness[J]. Journal of Propulsion Technology, 2013, 34(12): 1585-1592.)
[6] 南向军, 张堃元, 金志光, 等. 矩形转圆形高超声速内收缩进气道数值及试验研究[J]. 航空学报, 2011, 32(6): 988-996.
[7] Thomas T Y. On Curved Shock Waves[J]. Journal of Mathematics & Physics, 1947, 26(1): 62-68.
[8] Lin C C, Rubinov S I. On the Flow behind Curved Shocks[J]. Journal of Mathematics & Physics, 1948, 27(1): 105-129.
[9] Thomas T Y. The Consistency Relations for Shock Waves[J]. Journal of Mathematics & Physics, 1949, 28(1): 62-90.
[10] Truesdell C. On Curved Shocks in Steady Plane Flow of an Ideal Fluid[J]. Journal of the Aeronautical Sciences, 1952, 19(12): 826-828.
[11] Hayes W D. The Vorticity Jump across a Gasdynamic Discontinuity[J]. Journal of Fluid Mechanics, 1957, 2(2): 595-600.
[12] Kanwal R P. On Curved Shock Waves in Three-Dimensional Gas Flows[J]. Quarterly of Applied Mathematics, 1959, 16: 361-372.
[13] Darden C M. Spatial Derivatives of Flow Quantities behind Curved Shocks of All Strengths[R]. NASA TM 85782, 1984.
[14] M?lder S. Curved Shock Theory[J]. Shock Waves, 2016, 26: 337-353.
[15] 韩伟强, 朱呈祥, 尤延铖, 等. 二阶弯曲激波理论的推导与应用研究[C]. 哈尔滨:第八届全国高超声速科技学术会议, 2015.
[16] Sirovich L, Chong T H. Approximate Solution in Gasdynamics[J]. Physics of Fluids, 1980, 23: 1291.
[17] Lewis T S, Sirovich L. Approximate and Exact Numerical Computation of Supersonic Flow over an Airfoil[J]. Journal of Fluid Mechanics, 1981, 112.
[18] Sirovich L, Lewis T S. The Inverse Problem for Supersonic Airfoils[J]. AIAA Journal, 1984, 22(22): 295-297.
[19] Meyer R E. Theory of Characteristics of Inviscid Gasdynamics[J]. Handbuch Der Physik, 1960, (9): 225-282.
[20] Anderson John D. Fundamentals of Aerodynamics[M]. USA: McGraw-Hill Education, 2005. * 收稿日期:2016-05-25;修订日期:2016-11-02。基金项目:国家自然科学基金(51276151;91441128);国防基础科研(B1420133058);中央高校基本科研业务费 (20720140540)。作者简介:施崇广,男,硕士生,研究领域为高超声速气体动力学。E-mail: chongguang.shi@qq.com通讯作者:尤延铖,男,博士,教授,研究领域为高超声速推进系统设计。E-mail: yancheng.you@xmu.edu.cn(编辑:史亚红)
|