Numerical study of turbulent mixing processes in RQL gas turbine combustor
RNG (Renormalization Group) k-e turbulent model was applied to the numerical simulation of turbulent mixing processes in a RQL gas turbine combustor,and SIMPLE algorithm was used to solve the finite difference equations. Calculations are in agreement with experimental date. Based on the concept of equivalent isothermal flow,the mixing quality which is affected by the injector zone geometry and the jet to crossflow momentum flux ratios was discussed,through analysing the temperature fields of the flow and near-wall. The results indicated that the effect is obvious.
RQL combustor turbulence flow field RNG k-ε model temperature equivalent numerical simulation
Yu Liang Yuan Shu-sheng Wang Yun-liang Dong Yuan
Graduate Students brigade Naval Aeronautical and Astronautical University Yantai,China Department of Aerocraft Engineering Naval Aeronautical and Astronautical University Yantai,China Naval Meteorology and Oceanography Center Beijing,China
国际会议
杭州
英文
567-570
2012-03-23(万方平台首次上网日期,不代表论文的发表时间)