| Citation: | LU Heng, ZHANG Zhibin, XU Xiao, et al. Effect of inlet temperatures on pulse detonation combustion characteristics[J]. Journal of Aerospace Power, 2025, 40（6）：20230821 doi: 10.13224/j.cnki.jasp.20230821
|
In order to obtain the influence of inlet temperature on the pulse detonation combustion characteristics, the combustion state, peak pressure, pressure wave and flame propagation velocity in detonation tube were studied under the conditions of detonation ignition frequency of 15—25 Hz and inlet temperature of 300—450 K by means of experimental and theoretical analysis. The results showed that: from the experimental and theoretical analysis results, the peak pressure was inversely proportional to the inlet temperature; when the inlet temperature was 300 K, the overall flame propagation velocity was low, and the fastest reached
| [1] |
HEISER W H,PRATT D T. Thermodynamic cycle analysis of pulse detonation engines[J]. Journal of Propulsion and Power,2002,18(1): 68-76. doi: 10.2514/2.5899
|
| [2] |
于锦禄,何立明,丁未,等. 瞬态等离子体点火和火花塞点火起爆过程的对比研究[J]. 推进技术,2013,34(11): 1575-1579. YU Jinlu,HE Liming,DING Wei,et al. Comparative investigation on detonation initiation process of transient plasma ignition and spark ignition[J]. Journal of Propulsion Technology,2013,34(11): 1575-1579. (in Chinese
YU Jinlu, HE Liming, DING Wei, et al. Comparative investigation on detonation initiation process of transient plasma ignition and spark ignition[J]. Journal of Propulsion Technology, 2013, 34(11): 1575-1579. (in Chinese)
|
| [3] |
王永佳,范玮,高瞻,等. 脉冲爆震火箭发动机引射模态的起爆实验研究[J]. 推进技术,2013,34(8): 1147-1152. WANG Yongjia,FAN Wei,GAO Zhan,et al. Experimental study on the initiation of the ejection mode of the pulse detonation rocket engine[J]. Journal of Propulsion Technology,2013,34(8): 1147-1152. (in Chinese
WANG Yongjia, FAN Wei, GAO Zhan, et al. Experimental study on the initiation of the ejection mode of the pulse detonation rocket engine[J]. Journal of Propulsion Technology, 2013, 34(8): 1147-1152. (in Chinese)
|
| [4] |
SCHAUER F,MISER C,TUCKER C,et al. Detonation initiation of hydrocarbon-air mixtures in a pulsed detonation engine[R]. AIAA-2005-1343,2005.
|
| [5] |
于潇栋,王可,朱亦圆,等. 无阀模式下液态燃料高频爆震燃烧组织方法实验研究[J]. 航空学报,2022,43(12): 126245. YU Xiaodong,WANG Ke,ZHU Yiyuan,et al. Experimental study on liquid fueled high-frequency detonations in the valveless scheme[J]. Acta Aeronautica et Astronautica Sinica,2022,43(12): 126245. (in Chinese
YU Xiaodong, WANG Ke, ZHU Yiyuan, et al. Experimental study on liquid fueled high-frequency detonations in the valveless scheme[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(12): 126245. (in Chinese)
|
| [6] |
鲁唯. 脉冲爆震火箭发动机高频工作机理及控制规律研究[D]. 西安: 西北工业大学,2018. LU Wei. Study on high frequency working mechanism and control law of pulse detonation rocket engine[D]. Xi’an: Northwestern Polytechnical University,2018. (in Chinese
LU Wei. Study on high frequency working mechanism and control law of pulse detonation rocket engine[D]. Xi’an: Northwestern Polytechnical University, 2018. (in Chinese)
|
| [7] |
张启斌. 脉冲爆震火箭发动机流体喷管研究[D]. 西安: 西北工业大学,2019. ZHANG Qibin. Research on fluid nozzle of pulse detonation rocket engine [D]. Xi’an: Northwestern Polytechnical University,2019. (in Chinese
ZHANG Qibin. Research on fluid nozzle of pulse detonation rocket engine [D]. Xi’an: Northwestern Polytechnical University, 2019. (in Chinese)
|
| [8] |
何小民,王家骅. 圆环片扰流器对爆震燃烧特性的影响[J]. 航空动力学报,2005,20(6): 989-993. HE Xiaomin,WANG Jiahua. Disturber affect on the characteristics of detonation[J]. Journal of Aerospace Power,2005,20(6): 989-993. (in Chinese
HE Xiaomin, WANG Jiahua. Disturber affect on the characteristics of detonation[J]. Journal of Aerospace Power, 2005, 20(6): 989-993. (in Chinese)
|
| [9] |
王云,范明华,刘赛南,等. 障碍物对脉冲爆震火箭发动机性能影响的试验研究[J]. 推进技术,2021,42(4): 834-841. WANG Yun,FAN Minghua,LIU Sainan,et al. Experimental study on the influence of obstacles on the performance of pulse detonation rocket engine[J]. Journal of Propulsion Technology,2021,42(4): 834-841. (in Chinese
WANG Yun, FAN Minghua, LIU Sainan, et al. Experimental study on the influence of obstacles on the performance of pulse detonation rocket engine[J]. Journal of Propulsion Technology, 2021, 42(4): 834-841. (in Chinese)
|
| [10] |
BROPHY C,NETZER D,SINIBALDI J,et al. Operation of a JP10/air pulse detonation engine[R]. AIAA-2000-3591,2000.
|
| [11] |
SMIRNOV N N,NIKITIN V F,PHYLIPPOV Y G. Deflagration-to-detonation transition in gases in tubes with cavities[J]. Journal of Engineering Physics and Thermophysics,2010,83(6): 1287-1316. doi: 10.1007/s10891-010-0448-6
|
| [12] |
陈祥. 变截面管道内爆轰波起爆及传播特性研究[D]. 镇江: 江苏大学,2020. CHEN Xiang. Study on initiation and propagation characteristics of detonation wave in variable cross-section pipeline[D]. Zhenjiang: Jiangsu University,2020. (in Chinese
CHEN Xiang. Study on initiation and propagation characteristics of detonation wave in variable cross-section pipeline[D]. Zhenjiang: Jiangsu University, 2020. (in Chinese)
|
| [13] |
卢杰. 脉冲爆震涡轮发动机关键技术研究[D]. 西安: 西北工业大学,2016. LU Jie. Research on key technologies of pulse detonation turbine engine[D]. Xi’an: Northwestern Polytechnical University,2016. (in Chinese
LU Jie. Research on key technologies of pulse detonation turbine engine[D]. Xi’an: Northwestern Polytechnical University, 2016. (in Chinese)
|
| [14] |
LANDRY K,SHEHADEH R,BOUVET N,et al. Effect of operating frequency on PDE driven ejector thrust performance[R]. AIAA-2005-3832,2005.
|
| [15] |
COOPER M,JACKSON S,AUSTIN J,et al. Direct experimental impulse measurements for detonations and deflagrations[J]. Journal of Propulsion and Power,2002,18(5): 1033-1041. doi: 10.2514/2.6052
|
| [16] |
陈仁松,高新军. 温度和压力对燃料脉冲爆震参数的影响研究[C]//全国危险物质与安全应急技术研讨会论文集. 重庆: 中国工程物理研究院,2011: 310-314. CHEN Rensong,GAO Xinjun. Effect of temperature and pressure on pulse detonation parameters [C]//National Symposium on Hazardous Substances and Safety Emergency Technology. Chongqing : Chinese Academy of Engineering Physics,2011 : 310-314. (in Chinese
CHEN Rensong, GAO Xinjun. Effect of temperature and pressure on pulse detonation parameters [C]//National Symposium on Hazardous Substances and Safety Emergency Technology. Chongqing : Chinese Academy of Engineering Physics, 2011 : 310-314. (in Chinese)
|
| [17] |
朱旭东,范玮,范珍涔,等. 燃油温度对脉冲爆震火箭发动机比冲影响的实验研究[J]. 西北工业大学学报,2011,29(6): 955-959. ZHU Xudong,FAN Wei,FAN Zhencen,et al. Experimental investigations on effect of kerosene temperature on specific impulse of a pulse detonation rocket engine (PDRE)[J]. Journal of Northwestern Polytechnical University,2011,29(6): 955-959. (in Chinese doi: 10.3969/j.issn.1000-2758.2011.06.023
ZHU Xudong, FAN Wei, FAN Zhencen, et al. Experimental investigations on effect of kerosene temperature on specific impulse of a pulse detonation rocket engine (PDRE)[J]. Journal of Northwestern Polytechnical University, 2011, 29(6): 955-959. (in Chinese) doi: 10.3969/j.issn.1000-2758.2011.06.023
|
| [18] |
蒋弢,翁春生. 进气温度和当量比对脉冲爆轰发动机工作过程影响[J]. 航空动力学报,2015,30(1): 29-37. JIANG Tao,WENG Chunsheng. Effect of inlet temperature and equivalence ratio on working process of pulse detonation engine[J]. Journal of Aerospace Power,2015,30(1): 29-37. (in Chinese
JIANG Tao, WENG Chunsheng. Effect of inlet temperature and equivalence ratio on working process of pulse detonation engine[J]. Journal of Aerospace Power, 2015, 30(1): 29-37. (in Chinese)
|
| [19] |
GORDON S,MCBRIDE B. Computer program for calculation of complex chemical equilibrium compositions[J]. NASA Reference Publications,1996,1311(4): 441-443.
|
| [20] |
马国斌. 燃烧边界条件对自燃及爆震影响的实验研究[D]. 天津: 天津大学,2018. MA Guobin. Experimental study on the influence of combustion boundary conditions on spontaneous combustion and detonation[D]. Tianjin: Tianjin University,2018. (in Chinese
MA Guobin. Experimental study on the influence of combustion boundary conditions on spontaneous combustion and detonation[D]. Tianjin: Tianjin University, 2018. (in Chinese)
|
| [21] |
WANG Xin,CHEN Wanghua,DU Zhenhua. Influence of initial temperature and initial pressure on gas detonation parameters[J]. China Safety Science Journal,2010,37(6): 696-702.
|
| [22] |
韩启祥. 爆震机理及旋转阀脉冲爆震发动机原理样机研究[D]. 南京: 南京航空航天大学,2004. HAN Qixiang. Detonation mechanism and principle prototype of rotary valve pulse detonation engine [D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2004. (in Chinese
HAN Qixiang. Detonation mechanism and principle prototype of rotary valve pulse detonation engine [D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2004. (in Chinese)
|
| [23] |
翁春生,王杰,白桥栋,等. 脉冲爆轰发动机进气压力对爆轰影响的实验研究[J]. 弹道学报,2008,20(3): 1-4. WENG Chunsheng,WANG Jie,BAI Qiaodong,et al. Experimental study on effect of inlet pressure on detonation in pulse detonation engine[J]. Journal of Ballistics,2008,20(3): 1-4. (in Chinese
WENG Chunsheng, WANG Jie, BAI Qiaodong, et al. Experimental study on effect of inlet pressure on detonation in pulse detonation engine[J]. Journal of Ballistics, 2008, 20(3): 1-4. (in Chinese)
|
| [24] |
覃慧. 爆震波起爆瞬态过程现象和机理研究[D]. 长沙: 国防科技大学,2020. QIN Hui. Study on the phenomenon and mechanism of transient process of detonation wave initiation[D]. Changsha: National University of Defense Technology,2020. (in Chinese
QIN Hui. Study on the phenomenon and mechanism of transient process of detonation wave initiation[D]. Changsha: National University of Defense Technology, 2020. (in Chinese)
|
| [25] |
刘世铮. 丙烷气相爆燃转爆轰特性及机理研究[D]. 哈尔滨: 哈尔滨工程大学,2021. LIU Shizheng. Study on characteristics and mechanism of propane gas phase deflagration to detonation[D]. Harbin: Harbin Engineering University,2021. (in Chinese
LIU Shizheng. Study on characteristics and mechanism of propane gas phase deflagration to detonation[D]. Harbin: Harbin Engineering University, 2021. (in Chinese)
|
| [26] |
ALAM N,SHARMA K K,PANDEY K M. Effects of various compositions of the fuel-air mixture on the pulse detonation engine performance[J]. Combustion,Explosion,and Shock Waves,2019,55(6): 708-717. doi: 10.1134/S0010508219060121
|
| [27] |
张彭岗. 缓燃向爆震转捩特性研究[D]. 南京: 南京航空航天大学,2009. ZHANG Penggang. Study on transition characteristics of slow combustion to detonation[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2009. (in Chinese
ZHANG Penggang. Study on transition characteristics of slow combustion to detonation[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009. (in Chinese)
|
| [28] |
韩启祥,王家骅,王维来. 测量爆燃到爆震转捩距离的离子探针技术研究[J]. 航空动力学报,2003,18(1): 97-100. HAN Qixiang,WANG Jiahua,WANG Weilai. Investigation of the ion-probe technology for measuring the DDT distance[J]. Journal of Aerospace Power,2003,18(1): 97-100. (in Chinese doi: 10.3969/j.issn.1000-8055.2003.01.017
HAN Qixiang, WANG Jiahua, WANG Weilai. Investigation of the ion-probe technology for measuring the DDT distance[J]. Journal of Aerospace Power, 2003, 18(1): 97-100. (in Chinese) doi: 10.3969/j.issn.1000-8055.2003.01.017
|
| [29] |
王家骅,韩启祥. 脉冲爆震发动机技术[M]. 北京: 国防工业出版社,2013. WANG Jiahua,HAN Qixiang. Pulse detonation engine[M]. Beijing: National Defense Industry Press,2013. (in Chinese
WANG Jiahua, HAN Qixiang. Pulse detonation engine[M]. Beijing: National Defense Industry Press, 2013. (in Chinese)
|
| [30] |
何小民,张彭岗,王家骅. 爆震管内爆燃到爆震转捩过程的实验研究[J]. 推进技术,2005,26(3): 252-255,269. HE Xiaomin,ZHANG Penggang,WANG Jiahua. Experimental investigation of deflagration to detonation transition in two-phase mixture combustion[J]. Journal of Propulsion Technology,2005,26(3): 252-255,269. (in Chinese doi: 10.3321/j.issn:1001-4055.2005.03.014
HE Xiaomin, ZHANG Penggang, WANG Jiahua. Experimental investigation of deflagration to detonation transition in two-phase mixture combustion[J]. Journal of Propulsion Technology, 2005, 26(3): 252-255, 269. (in Chinese) doi: 10.3321/j.issn:1001-4055.2005.03.014
|
| [31] |
TURNS S R. 燃烧学导论: 概念与应用[M]. 姚强,李水清,王宇,译. 北京: 清华大学出版社,2015. TURNS S R. An introduction to combustion[M]. YAO Qiang,LI Shuiqing,WANG Yu,Translated. Beijing: Tsinghua University Press,2015. (in Chinese
TURNS S R. An introduction to combustion[M]. YAO Qiang, LI Shuiqing, WANG Yu, Translated. Beijing: Tsinghua University Press, 2015. (in Chinese)
|
DownLoad:
