Wall-Resolved Large-Eddy Simulation of Flow Over a Three-Dimensional Gaussian Bump

被引:0
|
作者
Rizzetta, Donald P. [1 ]
Garmann, Daniel J. [1 ]
机构
[1] Air Force Res Lab, Wright Patterson AFB, OH 45433 USA
关键词
Smooth-Body separation; Gaussian bump; large-eddy simulation; high-order numerical method; compact-differencing scheme; BOUNDARY-LAYER;
D O I
10.1080/10618562.2023.2246391
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Wall-resolved large-eddy simulations were carried out for the flow over a Gaussian bump configuration. The geometry and flow conditions were motivated by an experimental investigation, which was conducted in order to provide data for validating numerical modelling. The present computations were initiated as benchmark results that are accessible via wall-resolved large-eddy simulation. It was found that by increasing the bump height, the Reynolds number could be reduced and flow separation would occur. The modified bump then serves as a surrogate for the original Gaussian bump producing a smooth separated flow. Solutions to the unsteady three-dimensional compressible Navier-Stokes equations were obtained utilising a high-fidelity computational scheme and an implicit time-marching approach. Large-eddy simulations were performed and grid resolution studies were carried to ensure quality of computed results. Features of the flowfields are elucidated, and it was found that the time-mean surface streamline pattern had similar features to that of the experiment.
引用
收藏
页码:28 / 48
页数:21
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