Comparison of experiments and simulations for zero pressure gradient turbulent boundary layers at moderate Reynolds numbers

被引:0
作者
Ramis Örlü
Philipp Schlatter
机构
[1] KTH Mechanics,Linné FLOW Centre, Swedish e
来源
Experiments in Fluids | 2013年 / 54卷
关键词
Reynolds Number; Direct Numerical Simulation; Streamwise Velocity; Skin Friction Coefficient; Direct Numerical Simulation Data;
D O I
暂无
中图分类号
学科分类号
摘要
A detailed comparison between recent direct numerical simulation (DNS) and experiments of a turbulent boundary layer under zero pressure gradient at Reθ = 2,500 and 4,000 (based on the free-stream velocity and momentum-loss thickness) is presented. The well-resolved DNS is computed in a long spatial domain (Schlatter and Örlü in J Fluid Mech 659:116, 2010a), including the disturbance strip, while the experiments consist of single hot-wire probe and oil-film interferometry measurements. Remarkably, good agreement is obtained for integral quantities such as skin friction and shape factor, as well as mean and fluctuating streamwise velocity profiles, higher-order moments and probability density distributions. The agreement also extends to spectral/structural quantities such as the amplitude modulation of the small scales by the large-scale motion and temporal spectral maps throughout the boundary layer. Differences within the inner layer observed for statistical and spectral quantities could entirely be removed by spatially averaging the DNS to match the viscous-scaled length of the hot-wire sensor, thereby explaining observed differences solely by insufficient spatial resolution of the hot-wire sensor. For the highest Reynolds number, Reθ = 4,000, the experimental data exhibit a more pronounced secondary spectral peak in the outer region (y/δ99 = 0.1) related to structures with length on the order of 5–7 boundary layer thicknesses, which is weaker and slightly moved towards lower temporal periods in the DNS. The cause is thought to be related to the limited spanwise box size which constrains the growth of the very large structures. In the light of the difficulty to obtain “canonical” flow conditions, both in DNS and the wind tunnel where effects such as boundary treatment, pressure gradient and turbulence tripping need to be considered, the present cross-validation of the data sets, at least for the present Reθ-range, provides important reference data for future studies and highlights the importance of taking spatial resolution effects into account when comparing experiment and DNS. For the considered flow, the present data also provide quantitative guidelines on what level of accuracy can be expected for the agreement between DNS and experiments.
引用
收藏
相关论文
共 173 条
[21]  
Gad-el-Hak M(2010)Hot-wire spatial resolution issues in wall-bounded turbulence J Fluid Mech 657 335-10
[22]  
Chauhan KA(2004)Turbulent boundary layers and channels at moderate Reynolds numbers Theor Comput Fluid Dyn 18 391-196
[23]  
Monkewitz PA(1987)DNS and scaling laws from new symmetry groups of ZPG turbulent boundary layer flow J Fluid Mech 177 133-337
[24]  
Nagib HM(2010)Turbulence statistics in fully developed channel flow at low Reynolds number J Fluid Eng 132 094001-701
[25]  
DeGraaff DB(1990)Reynolds number dependence, scaling, and dynamics of turbulent boundary layers J Fluid Mech 219 119-474
[26]  
Eaton JK(2011)On accurately measuring statistics associated with small-scale structure in turbulent boundary layers using hot-wire probes Int J Heat Fluid Flow 32 1-770
[27]  
del Álamo JC(2012)Direct numerical simulation of a turbulent boundary layer up to Phys Fluids 24 035110-239
[28]  
Jiménez J(2010) = 2500 Science 329 193-110
[29]  
del Álamo JC(2010)Rare backflow and extreme wall-normal velocity fluctuations in near-wall turbulence Phys Fluids 22 065103-387
[30]  
Jiménez J(2009)Predictive model for wall-bounded turbulent flow J Fluid Mech 628 311-129