[1] Mitani T, Ueda S, Tani K, et al. Validation studies of scramjet nozzle performance[J]. Journal of Propulsion and Power, 1993, 9(5): 725-730.
[2] Baucco A R, Shanley K T, Bevies D. CFD validation study for internal performance of advanced SERN configurations, AIAA-2012-4223[R]. 2012.
[3] Edwards C L Q, Small W J, Weidner J P, et al. Studies of scramjet/airframe integration techniques for hypersonic aircraft, AIAA-1975-58[R]. 1975.
[4] Xu J L, Zhang Y H, Zhang K Y. Numerical simulation of single expansion ramp nozzle for scramjet on the off-design point[J]. Journal of Propulsion Technology, 2007, 28(3): 287-290.(in Chinese) 徐惊雷, 张艳慧, 张堃元. 超燃冲压发动机非对称喷管非设计状态性能计算[J]. 推进技术, 2007, 28(3): 287-290.
[5] Damira S K, Marathe A G, Sudhakar K, et al. Parametric optimization of single expansion ramp nozzle(SERN), AIAA-2006-5188[R]. 2006.
[6] Ge J H, Xu J L, Wang M T, et al. The prediction of flow separation in SERN[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(8): 1394-1399.(in Chinese) 葛建辉, 徐惊雷, 王明涛, 等. 非对称喷管流动分离的预测[J]. 航空学报, 2012, 33(8): 1394-1399.
[7] Bradford J E. Rapid prediction of afterbody nozzle performance in scream, AIAA-2002-3605[R]. 2002.
[8] Starkey R P. Off-design performance characterization of a variable geometry scramjet, AIAA-2005-3711[R]. 2005.
[9] Mirmirani M, Wu C, Clark A, et al. Modeling for control of a generic airbreathing hypersonic vehicle, AIAA-2005-6256[R]. 2005.
[10] Lederer R. Testing the actively cooled fully variable hypersonic demonstrator nozzle, AIAA-1996-4550[R]. 1996.
[11] Lederer R, Kruger W. Nozzle development as a key element for hypersonics, AIAA-1993-5058[R]. 1993.
[12] Zhang K Y, Zhang R X, Xu H. Investigation of single expansion ramp nozzle[J]. Journal of Propulsion Technology, 2001, 22(5): 380-382.(in Chinese) 张堃元, 张荣学, 徐辉. 非对称大膨胀比喷管研究[J]. 推进技术, 2001, 22(5): 380-382.
[13] Haid D, Gamble E J. Nozzle aftbody drag reduction using fluidics, AIAA-2004-3921[R]. 2004.
[14] Gamble E, Haid D. Improving off-design nozzle performance using fluidic injection, AIAA-2004-1206[R]. 2004.
[15] Gamble E J, DeFrancesco R, Haid D, et al. Fluid nozzle to improve transonic pitch and thrust performance of hypersonic vehicle, AIAA-2005-3501[R]. 2005.
[16] Rao G V R. Exhaust nozzle contour for optimum thrust[J]. Journal of Jet Propulsion, 1958, 38(6): 377-382.
[17] Shyne R J, Keith T G. Analysis and design of optimized truncated scarfed nozzles subject to external flow effect, AIAA-1990-2222[R]. 1990. |