A microscopic study of one-dimensional H2-O2 detonation using DSMC method
Yang C(杨超); Huang HJ(黄河激); Sun QH(孙泉华)
2019
会议日期23 July 2018 ~ 27 July 2018
会议地点University of StrathclydeGlasgow; United Kingdom;
英文摘要The global and local behaviors of detonation waves are affected by the thermo-chemical coupling process which requires the understanding at molecular level due to its microscopic complexity. In present study, one-dimensional H2-O2 detonation is numerically investigated through DSMC method. The detailed balance between forward and reverse reactions is achieved through a modified reaction model, which improves the simulation accuracy of combustion system. Results show that the overall structure of detonation is in accordance with the CFD result, but the microscopic fluctuation of auto-ignition affects detonation in both initiation and propagation stages. Analysis of the detailed structure in the induction zone shows that the auto-ignition process is strongly coupled with the vibrational relaxation process. The lower vibrational temperature decreases the chemical reaction rates, resulting in an increase of ignition delay time and induction zone length. © 2019 Author(s).
会议录AIP Conference Proceedings
语种英语
URL标识查看原文
ISBN号9780735418745
内容类型会议论文
源URL[http://dspace.imech.ac.cn/handle/311007/85088]  
专题力学研究所_高温气体动力学国家重点实验室
作者单位1.Laboratory for Aerospace Science and Technology, Institute of Mechanics, Chinese Academy of Sciences, Beijing, China
2.State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, CAS, Beijing, 100190, China
推荐引用方式
GB/T 7714
Yang C,Huang HJ,Sun QH. A microscopic study of one-dimensional H2-O2 detonation using DSMC method[C]. 见:. University of StrathclydeGlasgow; United Kingdom;. 23 July 2018 ~ 27 July 2018.
个性服务
查看访问统计
相关权益政策
暂无数据
收藏/分享
所有评论 (0)
暂无评论
 

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。


©版权所有 ©2017 CSpace - Powered by CSpace