[1] Lin Z M. The current development and future trends of fighter engines. Aeroengine, 2006, 32(1): 1-8. (in Chinese) 林左鸣. 战斗机发动机的研制现状和发展趋势. 航空发动机, 2006, 32(1): 1-8. [2] Shan Y, Zhang J Z, Shao W R, et al. Experiments on infrared radiation characteristics of exhaust system for a turbofan engine. Journal of Aerospace Power, 2009, 24(10): 2228-2234. (in Chinese). 单勇, 张靖周, 邵万仁, 等. 某型涡扇排气系统缩比模型红外辐射特性实验. 航空动力学报, 2009, 24(10): 2228-2234. [3] Carlson J R, Abdol-Hamid K S. Prediction of static performance for single expansion ramp nozzles. AIAA-1993-2571, 1993. [4] MacLean M K, GE Aircraft Engines, Cincinnati O H. Static internal performance tests of single expansion ramp nozzle concepts designed with LO considerations. AIAA-1993-2429, 1993. [5] Ruffin S M, Venkatapathy E, Lee S H, et al. Single expansion ramp nozzle simulations. AIAA-1992-0387, 1992. [6] Capone F J. The nonaxisymmetric nozzle-it is for real. AIAA-1979-1810, 1979. [7] Damira S K, Marathe A G, Sudhakar K, et al. Parametric optimization of single expansion ramp nozzle (SERN). AIAA-2006-5188, 2006. [8] Lee B J, Kin C, Rho O. Optimal shape design of the S-shaped subsonic intake using nurbs. AIAA-2005-455, 2005. [9] He X Z, Zhang Y, Wang G Y, et al. Automated design optimization of single expansion ramp nozzle for hypersonic vehicle. Journal of Propulsion Technology, 2007, 28(2): 148-151.(in Chinese) 贺旭照, 张勇, 汪广元, 等. 高超声速飞行器单壁膨胀喷管的自动优化设计. 推进技术, 2007, 28(2): 148-151. [10] Tan J, Jin J, Du G, et al. Experimental and computational investigation of an over-expanded single-expansion-ramp-nozzle. Journal of Propulsion Technology, 2009, 30(3): 293-296. (in Chinese) 谭杰, 金捷, 杜刚, 等. 过膨胀单边膨胀喷管实验和数值模拟. 推进技术, 2009, 30(3): 293-296. [11] Zhang K Y, Zhang R X, Xu H. Investigation of single expansion ramp nozzle. Journal of Propulsion Technology, 2001, 22(5): 381-382. (in Chinese) 张堃元, 张荣学, 徐辉. 非对称大膨胀比喷管研究. 推进技术, 2001, 22(5): 381-382. [12] Deere K A, Asbury S C. Experimental and computational investigation of a translation-throat single-expansion-ramp nozzle. NASA/TP 1999-209138, 1999. [13] Gamble E, Haid D. Improving off-design nozzle performance using fluidic injection. AIAA-2004-1206, 2004. [14] Marathe A G, Thiagarajan V. Effect of geometric parameters on the performances of single expansion ramp nozzle. AIAA-2005-4429, 2005. [15] Wang W N, Wang Z X, Qiao W Y. Investigation of the influence of single expansion ramp nozzle geometric parameters on the flow field and performance. Journal of Aerospace Power, 2006, 21(2): 281-284. (in Chinese) 汪维娜, 王占学, 乔渭阳. 单斜面膨胀喷管几何参数对流场和性能的影响. 航空动力学报, 2006, 21(2): 281-284. [16] Yang C Y, Zhang J Z, Shan Y. Numerical simulation on infrared radiation characteristics of single expansion ramp nozzles. Acta Aeronautica et Astronautica Sinica, 2010, 31(10): 1919-1926. (in Chinese) 杨承宇, 张靖周, 单勇. 单边膨胀喷管红外辐射特性的数值模拟. 航空学报, 2010, 31(10): 1919-1926. [17] Zhang S L, Shan Y, Zhang J Z. Numerical study on aerodynamic and infrared radiation characteristics of single expansion ramp nozzle. Journal of Aerospace Power, 2011, 26(7): 1502-1508. (in Chinese) 张少丽, 单勇, 张靖周. 单边膨胀喷管气动和红外辐射特性数值研究. 航空动力学报, 2011, 26(7): 1502-1508. [18] Shan Y, Zhang J Z, Li L G. Numerical calculation and experimental verification for the infrared characteristics of helicopter infrared radiation suppressor. Journal of Infrared and Millimeter Waves, 2006, 25(2): 96-100. (in Chinese) 单勇, 张靖周, 李立国. 直升机红外抑制器红外辐射特征的数值研究和实验验证. 红外与毫米波学报, 2006, 25(2): 96-100. [19] Shan Y, Zhang J Z. Numerical investigation of flow mixture enhancement and infrared radiation shield by lobed forced mixer. Applied Thermal Engineering, 2009, 29(17-18): 3687-3695. |