Numerical simulations of the formation and propagation of an <italic style="font-style: italic">n</italic>-decane/air rotating detonation wave

Xiaofeng SHAO; Ningbo ZHAO; Shizheng LIU; Qingyang MENG; Yajun LI; Hongtao ZHENG

doi:10.11990/jheu.202204003

Chinese

您当前的位置：

首页 >

文章列表页 >

Numerical simulations of the formation and propagation of an n-decane/air rotating detonation wave

更新时间：2025-09-01

- Numerical simulations of the formation and propagation of an n-decane/air rotating detonation wave
- Journal of Harbin Engineering University Vol. 45, Issue 4, Pages: 730-738(2024)
- 作者机构：
  
  1.哈尔滨工程大学动力与能源工程学院, 黑龙江哈尔滨 150001
  2.中国船舶集团有限公司第七〇三研究所, 黑龙江哈尔滨 150078
- 作者简介：
- 基金信息：
- DOI：10.11990/jheu.202204003
  CLC： V231.2
- Received：01 April 2022，
  
  Online First：19 February 2024，
  
  Published：05 April 2024
- 稿件说明：
移动端阅览
Xiaofeng SHAO, Ningbo ZHAO, Shizheng LIU, et al. Numerical simulations of the formation and propagation of an n-decane/air rotating detonation wave[J]. Journal of Harbin Engineering University, 2024, 45(4): 730-738.
DOI：

Xiaofeng SHAO, Ningbo ZHAO, Shizheng LIU, et al. Numerical simulations of the formation and propagation of an n-decane/air rotating detonation wave[J]. Journal of Harbin Engineering University, 2024, 45(4): 730-738. DOI： 10.11990/jheu.202204003.

摘要

针对气液两相旋转爆轰波形成与传播问题

本文以液态正癸烷为燃料

采用欧拉-拉格朗日方法

通过三维数值模拟给出了两相旋转爆轰波的形成演变特点和自持传播机理。研究结果表明: 在起爆阶段

通过调控初始燃料分布能够获得强度不同的爆轰波和压力波; 在对撞阶段

爆轰波与压力波共发生4次对撞

由于缺乏燃料供给

压力波逐渐衰减并消失

爆轰波以单波模态传播; 在稳定传播阶段

未燃燃料在三叉点处聚集形成未反应气流区并诱导产生局部爆炸。未反应气流区的周期性出现和局部爆炸是两相爆轰波自持传播的重要影响因素。

Abstract

To investigate the formation and propagation of a gas-liquid two-phase rotating detonation wave

three-dimensional numerical simulations were conducted to discuss the formation and evolution characteristics and self-sustaining propagation mechanism of

-decane/air rotating detonation wave using the Euler-Lagrangian method. The results reveal that the detonation and pressure waves with different intensities can be obtained by adjusting the initial fu

el distribution during the ignition stage. In the collision stage

four collisions occurred between the detonation and pressure waves. Owing to the lack of fuel supply

the pressure wave gradually decayed and disappeared

and the detonation wave propagated in a single-wave mode. In the stable propagation stage

the unburned fuel accumulated at the contact triple point to form an unreacted gas flow region and a local explosion was induced. The periodic occurrence of the unreacted gas flow region and local explosion are important factors affecting the self-sustained propagation of two-phase detonation waves.

关键词

Keywords

references

ANAND V, GUTMARK E. Rotating detonation combustors and their similarities to rocket instabilities[J]. Progress in energy and combustion science, 2019, 73: 182-234.

WOLAŃSKI P. Detonative propulsion[J]. Proceedings of the combustion institute, 2013, 34(1): 125-158.

ZHAO Majie, ZHANG Huangwei. Origin and chaotic propagation of multiple rotating detonation waves in hydrogen/air mixtures[J]. Fuel, 2020, 275: 117986.

LIU Shizheng, CHEN Xiang, ZHAO Ningbo, et al. Experimental study on initiation and propagation behavior of propane/oxygen/nitrogen detonation wave[J]. Fuel, 2021, 293: 120487.

王宇辉, 王超, 郑榆山, 等. 基于乙烯或氢气的吸气式旋转爆轰发动机实验[J]. 气体物理, 2018, 3(6): 16-25.

WANG Yuhui, WANG Chao, ZHENG Yushan, et al. Experimental on air-breathing rotating detonation engine using ethylene or hydrogen[J]. Physics of gases, 2018, 3(6): 16-25.

BYKOVSKⅡ F A, ZHDAN S A, VEDERNIKOV E F. Continuous spin detonations[J]. Journal of propulsion and power, 2006, 22(6): 1204-1216.

BYKOVSKⅡ F A, ZHDAN S A, VEDERNIKOV E F. Continuous detonation of the liquid kerosene—air mixture with addition of hydrogen or syngas[J]. Combustion, explosion, and shock waves, 2019, 55(5): 589-598.

BYKOVSKⅡ F A, ZHDAN S A, VEDERNIKOV E F. Continuous spin detonation of a heterogeneous kerosene-air mixture with addition of hydrogen[J]. Combustion, explosion, and shock waves, 2016, 52(3): 371-373.

KINDRACKI J. Experimental studies of kerosene injection into a model of a detonation chamber[J]. Journal of power technologies, 2012, 92(2): 80-89.

KINDRACKI J. Experimental research on rotating detonation in liquid fuel-gaseous air mixtures[J]. Aerospace science and technology, 2015, 43: 445-453.

郑权, 李宝星,翁春生, 等. 燃烧室长度对液态燃料旋转爆轰发动机性能影响实验研究[J]. 推进技术, 2018, 39(12): 2764-2771.

ZHENG Quan, LI Baoxing, WENG Chunsheng, et al. Experimental investigation for effects of combustor length on liquid-fueled rotating detonation engine performance[J]. Journal of propulsion technology, 2018, 39(12): 2764-2771.

郑权, 魏万里, 翁春生, 等. 液态燃料喷注压力对旋转爆轰波影响的实验研究[J]. 推进技术, 2020, 41(12): 2790-2797.

ZHENG Quan, WEI Wanli, WENG Chunsheng, et al. Experimental study for effects of liquid-fuel injection pressure on rotating detonation wave[J]. Journal of propulsion technology, 2020, 41(12): 2790-2797.

郑权, 翁春生, 白桥栋. 当量比对液体燃料旋转爆轰发动机爆轰影响实验研究[J]. 推进技术, 2015, 36(6): 947-952.

ZHENG Quan, WENG Chunsheng, BAI Qiaodong. Experimental study on effects of equivalence ratio on detonation characteristics of liquid-fueled rotating detonation engine[J]. Journal of propulsion technology, 2015, 36(6): 947-952.

MENG Qingyang, ZHAO Majie, ZHENG Hongtao, et al. Eulerian-lagrangian modelling of rotating detonative combustion in partially pre-vaporized n-heptane sprays with hydrogen addition[J]. Fuel, 2020.318-332.

MENG Qingyang, ZHAO Ningbo, ZHANG Huangwei. On the distributions of fuel droplets and in situ vapor in rotating detonation combustion with prevaporized n-heptane sprays[J]. Physics of fluids, 2021, 33(4): 043307.

HAYASHI A K, TSUBOI N, DZIEMINSKA E. Numerical study on JP-10/air detonation and rotating detonation engine[J]. AIAA journal, 2020, 58(12): 5078-5094.

SUN Bo, MA Hu. Two-dimensional numerical study of two-phase rotating detonation wave with different injections[J]. AIP advances, 2019, 9(11): 115307.

徐高, 翁春生, 康楠, 等. 考虑燃料雾化的气液两相连续旋转爆轰数值模拟[J]. 推进技术, 2022, 43(1): 181-189.

XU Gao, WENG Chunsheng, KANG Nan, et al. Numerical simulation of gas-liquid two-phase continuous rotating detonation considering fuel atomization[J]. Journal of propulsion technology, 2022, 43(1): 181-189.

REITZ R D, BEALE J C. Modeling spray atomization with the kelvin-helmholtz/rayleigh-taylor hybrid model[J]. Atomization and sprays, 1999, 9(6): 623-650.

WANG Yuhui, WANG Jianping, QIAO Wenyou. Effects of thermal wall conditions on rotating detonation[J]. Computers&fluids, 2016, 140: 59-71.

JIA Xiongbin, ZHAO Ningbo, LIU Shizheng, et al. Numerical investigation of detonation initiation for low-volatility liquid fuel/air mixtures[J]. Aerospace science and technology, 2021, 113: 106690.

雷知迪, 陈正武, 杨小权, 等. 调控燃烧室燃料初始分布建立稳定旋转爆轰波的方法[J]. 爆炸与冲击, 2019, 39(9): 4-14.

LEI Zhidi, CHEN Zhengwu, YANG Xiaoquan, et al. Method based on controlling initial fuel distribution to establish stable rotating detonation wave in combustion chamber[J]. Explosion and shock waves, 2019, 39(9): 4-14.

SHEPHERD J. California Institute of Technology, Shock and detonation Toolbox-2021 version[EB/OL ] . https://shepherd.caltech.edu/EDL/PublicResources/sdt/ https://shepherd.caltech.edu/EDL/PublicResources/sdt/ .

REN Zhaoxin, ZHENG Longxi. Numerical study on rotating detonation stability intwo-phase kerosene-air mixture[J]. Combustion and flame, 2021, 231: 111484.

WEN Haocheng, WEI Wei, FAN Wenqi, et al. On the propagation stability of droplet-laden two-phase rotating detonation waves[J]. Combustion and flame, 2022, 244: 112271.

LIM D, HUMBLE J, HEISTER S D, Experimental testing of an RP-2-GOX rotating detonation rocket engine[C]//AIAA SciTech Forum. Orlando, 2020: 0195.

ZHONG Yepan, WU Yun, JIN Di, et al. Investigation of rotating detonation fueled by the pre-combustion cracked kerosene[J]. Aerospace science and technology, 2019, 95: 105480.

HAN Jiaxiang, BAI Qiaodong, ZHANG Shijian, et al. Experimental study on propagation characteristics of rotating detonation wave with kerosene fuel-rich gas[J]. Defence technology, 2022, 18(8): 1498-1512.

BLUEMNER R, BOHON M D, PASCHEREIT C O, et al. Counter-rotating wave mode transition dynamics in an RDC[J]. International journal of hydrogen energy, 2019, 44(14): 7628-7641.

XIA Zhijie, TANG Xinmeng, LUAN Mingyi, et al. Numerical investigation of two-wave collision and wave structure evolution of rotating detonation engine with hollow combustor[J]. International journal of hydrogen energy, 2018, 43(46): 21582-21591.

李宝星, 翁春生. 气体与液体两相连续旋转爆轰发动机爆轰波传播特性三维数值模拟研究[J]. 兵工学报, 2017, 38(7): 1358-1367.

LI Baoxing, WENG Chunsheng. Three-dimensional numerical simulation on the propagation characteristics of detonation wave in gas-liquid two-phase continuous rotating detonation engine[J]. Acta armamentarii, 2017, 38(7): 1358-1367.

赵家丰, 聂万胜, 仝毅恒, 等. 喷注角度对超声速气流中液体横向射流的影响[J]. 推进技术, 2022, 43(6): 239-249.

ZHAO Jiafeng, NIE Wansheng, TONG Yiheng, et al. Effects of injection angles on liquid jets in supersonic crossflows[J]. Journal of propulsion technology, 2022, 43(6): 239-249.

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Numerical analysis of surface piercing propeller cup section's water exit and entry

Characteristic research on the flow and sound fields of the pump-jet-propelled submarine under cruising conditions

Aerodynamic interference characteristics and wind resistance optimization of the container ship superstructure

An analysis of blockage effect on the hydrodynamic performance of a horizontal axis tidal current turbine

Analysis of hydrodynamic characteristics of oblique flow angle to semisubmerged blade profile

Related Author

Cong SUN

Shengming CHANG

Hao WEI

Chao WANG

Rennian LI

Qiannian WANG

Renhui ZHANG

Zhourui LI

Related Institution

College of Shipbuilding Engineering, Harbin Engineering University

National Key Laboratory on Vibration & Noise, China Ship Scientific Research Center

College of Energy and Power Engineering, Lanzhou University of Technology

Key Laboratory of Fluid Machinery and Systems of Gansu Province

School of Ocean Engineering, Harbin Institute of Technology

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰

Numerical simulations of the formation and propagation of an n-decane/air rotating detonation wave

DOI：10.11990/jheu.202204003

摘要

Abstract

关键词

Keywords

references