Research Status and Prospect of Transition Technology

Journal of Propulsion Technology ›› 2015, Vol. 36 ›› Issue (11): 1624-1632.

Previous Articles Next Articles

Research Status and Prospect of Transition Technology

School of Energy and Power Engineering，Beijing University of Aeronautics and Astronautics，Beijing 100191，China,School of Energy and Power Engineering，Beijing University of Aeronautics and Astronautics，Beijing 100191，China,School of Power and Energy，Northwestern Polytechnical University，Xi’an，710072，China and School of Energy and Power Engineering，Beijing University of Aeronautics and Astronautics，Beijing 100191，China

Published:2021-08-15

冲压发动机转级技术研究现状与展望

郭昆¹,唐海龙¹,何勇攀²,张　坤¹

北京航空航天大学能源与动力工程学院，北京 100191,北京航空航天大学能源与动力工程学院，北京 100191,西北工业大学动力与能源学院，陕西西安 710072,北京航空航天大学能源与动力工程学院，北京 100191

作者简介:郭昆(1976—)，男，博士生，研究领域为发动机总体技术。

Abstract

Abstract: The transition technology of ramjets is a critical problem for the development of supersonic and hypersonic vehicles. The research status of the transition technology for ramjets，the selections of different aerodynamic schemes，inlet flow analysis technology，and transition time sequence design method during the ramjets’transition process are reviewed. Recent progress in this aspect are reviewed. Problems in recent research on scramjets’transition technology，numerical simulation and ground tests are pointed out. At last，prospects on the future study of this technology were presented.

Key words: Transition technology；Ramjet；Scramjet；Research status

摘要： 冲压发动机的转级技术是各类超声速、高超声速飞行器研制所面临的一类技术难题。为了系统性地研究冲压发动机转级技术的研究现状，总结了冲压发动机在转级过程气动方案设计、进气道流动分析、转级时序设计等方面所面临的关键技术问题，综述了国内外研究进展情况，在此基础上指出了当前在超燃冲压发动机转级技术研究、转级过程数值仿真、地面试验等方面存在的不足，对后续研究工作进行了展望。

关键词: 转级技术；亚燃冲压发动机；超燃冲压发动机；研究现状

GUO Kun¹,TANG Hai-long¹,HE Yong-pan²,ZHANG Kun¹. Research Status and Prospect of Transition Technology[J]. Journal of Propulsion Technology, 2015, 36(11): 1624-1632.

郭昆,唐海龙,何勇攀,张　坤. 冲压发动机转级技术研究现状与展望[J]. 推进技术, 2015, 36(11): 1624-1632.

References

[1] 刘兴洲主编. 飞航导弹动力装置[M]. 北京:宇航出版社, 1992.
[2] Second X-51 Hypersonic Flight Ends Prematurely[J]. Flight International, 2011, 6, 15.
[3] 刘占生, 张云峰, 田新. 冲压发动机超声速进气道流动自激振荡研究[J]. 航空动力学报, 2008, 23( 9).
[4] Faulkner R F. The Evolution of the Hyset Hydrocarbon Fueled Scramjet Engine[R]. AIAA 2003-7005.
[5] Hank J M, Murphy J S, Mutzman R C. The X-51A Scramjet Engine Flight Demonstration Program [R]. AIAA 2008-2540.
[6] 温杰. 美国海军的HyFly计划 [J]. 飞航导弹, 2008, 12: 10-13.
[7] Hass N E, Smart M K, Paull A. Flight Data Analysis of Hyshot2 [R]. AIAA 2005-3354.
[8] 张国宏, 黄少波, 崔金平, 等. 固体火箭冲压发动机转级技术[J].弹箭与制导学报, 2012, 32(3): 129-132.
[9] Guido K, Christoph B. Air Intake Development for Supersonic Missiles[R]. AIAA 2008-5263.
[10] 谭慧俊, 郭荣伟, 万大为. 一种固冲组合发动机进气道通气减阻方案的特性研究[J]. 宇航学报, 2003, 24(2): 185-189.
[11] David E, Reubush L T, Vincent L R. Review of X-43A Return to Flight Activities and Current Status[R]. AIAA 2003-7085.
[12] 王翼. 高超声速进气道启动问题研究[D]. 长沙:国防科学技术大学, 2008.
[13] Charles Lee Dailey. Supersonic Diffuser Instability[J]. Journal of the Aeronautical Sciences, 1955, 22(2): 132-144.
[14] Hirschen C, Hermann D, Gülhan A, et al. Experimental Investigations of the Performance and Unsteady Behavior of a Supersonic Intake[J]. Journal of Propulsion and Power, 2007, 18(4): 566-574.
[15] Hermann D, Triesch K, Gülhan A, et al. Experimental Study of of Chin Intakes for Airbreathing Missiles with High Agilty[J]. Journal of Propulsion and Power, 2008, 24(2): 236-244.
[16] Weinreich H L, G m b Ottobrum. One-Dimensional Non-Linear Considerations on Supersonic Diffuser Buzz[R]. AGARD Conference Proceedings, 1981- AGARD-CP-307-12.
[17] Tan H J, Sun S. Oscillatory Flows of Rectangular Hypersonic Inlet Unstart Caused by Downstream Mass-Flow Choking[J]. Journal of Propulsion and Power, 2009, 25(1): 138-147.
[18] 白晓征, 刘君, 郭正, 等. 冲压发动机进气道压力振荡过程的数值研究[J]. 推进技术, 2008, 29(5): 562-565. (BAI Xiao-zheng, LIU Jun, GUO Zheng. Numerical Simulation of Pressure Oscillation in Ramjet Inlet[J]. Journal of Propulsion Technology, 2008, 29(5):562-565.)
[19] 李强, 刘佩进, 李江, 等. 冲压发动机助推段压强振荡现象数值分析[J]. 推进技术, 2008, 29 (6). (LI Qiang, LIU Pei-jin, LI Jiang, et al. Numerical Simulation of Boosting Stage Pressure Oscillation in Ramjet [J]. Journal of Propulsion Technology, 2008, 29(6).)
[20] 杨石林, 张晓旻, 齐红亮, 等. 固冲发动机转级过程中进气道动态特性分析[J]. 中国科学: 技术科学, 2015, 45(1): 25-30.
[21] 孟宇鹏, 朱守梅, 闫晓娜. 出口封闭的冲压发动机进气道激波振荡现象[J]. 推进技术, 2011, 32(5): 606-610. (MENG Yu-peng, ZHU Shou-mei, YAN Xiao-na. Shock Wave Oscillation for Outlet-Closed Ramjet Inlet[J]. Journal of Propulsion Technology, 2011, 32(5): 606-610.)
[22] 何勇攀, 陈玉春, 李立翰. 整体式固体火箭冲压发动机转级过程数值仿真[J].计算机仿真, 2015, 32(3): 119-122.
[23] Sterbentz William H, Evvard John C. Criterions for Prediction and Control of Ramjet Flow Pulsations[R]. NACA TN3506, 1955.
[24] 鲍文, 常军涛, 郭新刚, 等. 超燃冲压发动机进气道不起动仿真研究[J].航空动力学报, 2005, 20(5): 731-735.
[25] 王翼, 范晓樯, 梁剑寒, 等. 三维侧压高超声速进气道不启动流场试验与数值模拟研究[J]. 宇航学报 2008, 29(6): 1927-1931.
[26] 袁化成, 梁德旺. 高超声速侧压式模型进气道不起动特性分析[J]. 南京航空航天大学学报, 2004, 36(6): 683-687.
[27] 李存杰. 整体式冲压发动机的几项关键技术问题[J].飞航导弹, 1992, 10(4): 37-41.
[28] 张家骅, 胡顺楠, 顾炎武, 等. 整体式固体火箭冲压发动机研制[J]. 推进技术, 1998, 19(2): 9-13. (ZHANG Jia-hua, HU Shun-nan, GU Yan-wu, et al. Development of an Integral Solid Rocket Ramjet Engine[J]. Journal of Propulsion Technology, 1998, 19(2): 9-13.)
[29] 黄少波. 整体式固冲发动机转级控制模块设计[J]. 航空兵器, 2009 (4): 58-64.
[30] Hong G S, Shih-Yang H, Vigor Y . A Unified Analysis of Ramjet Operation in an Integrated Rocket Ramjet Engine[R]. AIAA 2001-3460.
[31] Hong G S, Vigor Y . Unified Analysis of Internal Flowfield in an Integrated Rocket Ramjet Engine. II: Ramjet Sustainer[J]. Journal of Aerospace Engineering, 2014, 27(2): 398-403.
[32] 柳长安, 吴宝元, 王玉峰. 冲压发动机转级流场数值仿真研究[J]. 火箭推进, 2007, 33(5): 18-21.
[33] 何勇攀, 陈玉春, 李立翰. 冲压发动机进气道堵盖碎块运动仿真研究[J]. 计算机仿真, 2015, 32(5): 28-32.
[34] 何德胜, 李广武, 杨威, 等. 固冲发动机三工况转级试验气流转换装置设计[J]. 固体火箭技术, 2012, 35(3): 419-422. (编辑:朱立影)　　　　　　　　　　　　　*　收稿日期:2015-06-08；修订日期:2015-08-31。作者简介:郭昆(1976—),男,博士生,研究领域为发动机总体技术。E-mail: wwwwguokun@163.com

Research Status and Prospect of Transition Technology

冲压发动机转级技术研究现状与展望

PDF

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 0

Recommended Articles

Metrics

Comments