Numerical simulation of transverse jet flow field under supersonic inflow

摘要：

　　Transverse jet flow field under supersonic inflow is simulated numerically for studying the characteristic of fuel transverse jet and fuel mixing in scramjet combustion chamber.Comparison is performed between simulated results and the results of references and experiments.Results indicate that the CFD code in this paper is applicable for simulation of transverse jut flow field under supersonic inflow,but in order to providing more effective numerical predictive method,CFD code should be modified through increasing mesh density and adding LES module.

关键词： supersonic inflow transverse jet fuel mixing numerical simulation

作者: LI Qian WANG Dian-kai YANG Yin-jun FANG Juan

作者单位: State Key Laboratory of Laser Propulsion & Application,Space Engineering University,Beijing 101416,C Xichang Satellite Launch Center of China,Xichang Sichuan,615606 Jiuquan Satellite Launch Center of China,Jiuquan Gansu,732750

会议类型: 国际会议

会议名称: 2017第三届机械、电子和信息技术工程国际会议(ICMITE 2017)

会议地点: 成都

会议语种:英文

页码: 1-4

在线出版日期: 2017-12-16（万方平台首次上网日期，不代表论文的发表时间）