Effect of Primary Gas Entrance Angle on Specific Impulse of Water Ramjet
Received date: 2017-01-13
Online published: 2025-05-22
晁侃 , 牛楠 , 陆贺建 . 一次燃气入口角度对水冲压发动机比冲性能影响分析[J]. 弹箭与制导学报, 2017 , 37(5) : 87 -90,98 . DOI: 10.15892/j.cnki.djzdxb.2017.05.020
In order to investigate the effect of primary gas entrance angle on engine performance of water ramjet, based on eddy dissemination model, a 3-D multi-phase non-premixed combustion reaction model was established in a high level magnesium-based water ramjet, the influence of gas entrance angle on temperature distribution, variety of the mass fraction of magnesium in the afterburning chamber and specific impulse of water ramjet were also obtained. The numerical results show that several stream primary gases impacting in the center of water ramjet obviously increases magnesium-water reaction rate in the primary water penetration region, efficiently improves operating pressure and specific impulse of water ramjet, and also benefits for shortening the length of the afterburning chamber for the magnesium-water complete reaction.
| [1] | STINBRING D R, COOK R B, DZIELSKI J E, et al. High-speed supercavitating vehicles: AIAA 2006-6441[R]. Redstone: AIAA, 2006. |
| [2] | KO H, PARK B H, YOON W S. Evolutions of combusting flow in rocket-ramjet transition pegime: AIAA 2005-3506[R]. Redstone: AIAA, 2005. |
| [3] | RISHA G A. Combustion of Aluminum paticles with steam and liquid water: AIAA 2006-1154[R]. Redstone: AIAA, 2006. |
| [4] | TAHSINI A M, EBRAHIMI M. Increasing isp by injecting water into combustion chamber of an underwater SRM: AIAA 2006-4959[R]. Redstone: AIAA, 2006. |
| [5] | MIYAYAMA T, OSHIMA H, TOSHIYUKI S, et al. Improving combustion of boron particles in secondary combustor of ducted rockets: AIAA 2006-5250[R]. Redstone: AIAA, 2006. |
| [6] | ERMAKOV V A, RAZDOBREEV A A, SKORIK A I, et al. Temperature of aluminum particles at the time of ignition and combustion[J]. Combustion Explosion and Shock Waves, 1982, 18(2): 256 － 257. |
| [7] | MILIER T F, HERR J D. Green rocket propulsion by reaction of Al and Mg powders and water: AIAA 2004-4037[R]. Redstone: AIAA, 2004. |
| [8] | MIILER T F, WALTER J L, KIELY D H. A next-generation AUV energy system based on aluminum-seawater combustion[C]//IEEE. Proceedings of the symposium on Autonomous Underwater Vehicle Technology[ S. l.: s. n.], 2002: 111-119. |
| [9] | MILLER T F, GARZA A B. Finite rate calculations of magnesium combustion in vitiated oxygen and steam atmospheres: AIAA 2006-4066[R]. Redstone: AIAA, 2006. |
| [10] | 黄利亚, 夏智勋, 胡建新, 等. 镁基水冲压发动机燃烧室长度及进水距离设计方法[J]. 航空学报, 2001, 32(1): 67-74. |
| [11] | 朱千稳, 刘冰, 夏智勋, 等. 喷嘴特性对水冲压发动机性能的影响[J]. 导弹与航天运载技术, 2010 (6): 10-13. |
| [12] | 韩超, 夏智勋, 胡建新, 等. 水滴雾化直径对水冲压发动机比冲性能影响分析[C]//中国航空学会动力分会火箭发动机专业委员会. 2009 年会议论文集.出版地不详］:[出版者不祥］. 2009, 47-51. |
| [13] | 韩超, 夏智勋, 胡建新, 等. 一次进水角度对水冲压发动机比冲性能影响研究[J]. 固体火箭技术, 2009, 32(5): 496-499. |
| [14] | 韩超, 夏智勋, 胡建新, 等. 水燃比对水冲压发动机性能影响数值模拟与试验研究[J]. 国防科技大学学报, 2009, 31(4) :117-121. |
/
| 〈 |
|
〉 |