RNG(renormalization group)k-εmodel和代数应力模型(algebraic stress model))及算法(SI MPLE(semi-i mplicitmethod for pressure-linked equations)
PISO(pressure i mplicit split-operator))对复杂流场求解准确性及效率的影响.火焰筒三维贴体网格采用型线定点与偏微分方程相结合的方式生成
用壁面函数法处理近壁区域流动.计算结果表明
PISO算法提高求解效率;不同紊流模型预测结果均与试验数据符合较好
其中代数应力模型最为准确
更适用于复杂流场的数值预测.
Abstract
Three-dimension turbulence flow field in an annular combustor with two-stage radial swirler was simulated to quantify the prediction accuracy of different turbulent models(standard k-ε model
RNG(renormalization group) k-ε model
algebraic stress model) and the calculation efficiency of different algorithms(SIMPLE(semi-implicit method for pressure-linked equations) and PISO(pressure implicit split-operator)) in the complex flow fields.Body-fitted grid of the flametube used in this study was generated by an elliptical grid generation technique combined with the anchored grid method
and the flow fields near the wall were treated by the standard wall function.Computational results show that
PISO algorithm can be used to obtain an obviously higher efficiency.Simulation results gained from different turbulence models are in agreement with the experimental data.Among these turbulence models
the algebraic stress model is likely to offer better prediction capability for complex turbulent flow field.
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Related Author
WU Yao-zeng
HUANG Yong
WANG Fang
ZHANG Yu-fang
JI Hong-hu
ZHANG Jing-zhou
LIANG Bo
Ping ZHANG
Related Institution
School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Power and Energy,Northwestern Polytechnical University
Nondestructive Testing and Evaluation Laboratory, Dalian University of Technology
College of Civil Engineering, Hefei University of Technology
Key Laboratory of Aerospace Chemical Power Technology, Hubei Institute of Aerospace Chemical Techologh, China Aerospace Science and Technology Corporation,Xiangyang Hubei