Numerical simulation of effusion cooling with comparisons to experimental data

被引:5
|
作者
Gustafsson, KMB [1 ]
Johansson, TG
机构
[1] Volvo Aero Corp, Dept Aerothermodynam, SE-46181 Trollhattan, Sweden
[2] Chalmers Univ Technol, Dept Appl Mech, Div Fluid Dynam, SE-41296 Gothenburg, Sweden
来源
关键词
jet in crossflow; effusion cooling; film cooling; laser-Doppler anemometry; LDA; CFD; turbulence modelling; SST-kappa-omega; realisable kappa-epsilon; RSM;
D O I
10.1504/PCFD.2006.009487
中图分类号
O414.1 [热力学];
学科分类号
摘要
CFD simulations of a slanted jet in crossflow were made and compared to detailed 3D-LDA measurements. Three turbulence models were studied using Fluent v6.1: realisable k-epsilon, SST-k-omega and Reynolds stress model (RSM). The SST-k-omega model and the RSM were both able to capture the recirculation zone in the jet wake., which was not the case with the realisable k-epsilon model. The turbulent kinetic energy field was not well predicted by the k-epsilon or the SST-k-omega model. However, the Reynolds stress field was captured qualitatively correct by the RSM.
引用
收藏
页码:101 / 109
页数:9
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