Investigation of Coupling and Interacting between the Condensation Shock and Aerodynamic Shock in the Supersonic Non-Equilibrium Steam Flow
The supersonic non-equilibrium steam flow with spontaneous condensation and condensation shock was numerically studied based on the computational fluid dynamics method. A conservative compressible numerical model coupling with non-isothermal classical nucleation model was developed and used to predict the spontaneous condensation phenomenon with homogenous nucleation in supersonic steam flow. The improved high resolution Roe-FDS scheme was used to capture the transient characteristics of the condensation shock and the aerodynamic shock in the supersonic turbulent flow. Based on the simulation, the process of formation of the condensation shock was revealed, and the coupling and interacting between the condensation shock and aerodynamic shock were investigated, hi the study, the difference between the condensation shock and the aerodynamic shock was investigated, and the influence of the aerodynamic shock on the non-equilibrium phase change and condensation shock was revealed. In addition, the counteraction of the homogenous condensation on the aerodynamic shock was also studied.
Non-Equilibrium Steam Flow Condensation Shock Aerodynamic Shock Coupling Effect Interacting Effect
Yong Yang Shengqiang Shen Guohai Dong Song Guo Kunyu Wang
Key Laboratory for Desalination of Liaoning Province, Dalian University of Technology, Dalian, China Key Laboratory for Desalination of Liaoning Province, Dalian University of Technology, Dalian, China School of Hydraulic Engineering, Dalian University of Technology, Dalian, China
国际会议
The 7th International Conference on Fluid and Thermal Energy Conversion(第七届流动技术与热能转化国际会议 FTEC 2011)
郑州
英文
292-305
2011-09-24(万方平台首次上网日期,不代表论文的发表时间)