Implicit Subgrid-Scale Modeling of a Mach 2.5 Spatially Developing Turbulent Boundary Layer

被引:4
|
作者
Araya, Guillermo [1 ]
Lagares, Christian [1 ]
机构
[1] Univ Puerto Rico, Dept Mech Engn, High Performance Comp & Visualizat Lab, Mayaguez, PR 00681 USA
基金
美国国家科学基金会;
关键词
iLES; SUPG; supersonic; turbulent inflow conditions; boundary layers; LARGE-EDDY SIMULATION; DIRECT NUMERICAL-SIMULATION; CHANNEL FLOWS; REGION; PARALLEL; GALERKIN; FIELD;
D O I
10.3390/e24040555
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
We employ numerically implicit subgrid-scale modeling provided by the well-known streamlined upwind/Petrov-Galerkin stabilization for the finite element discretization of advection-diffusion problems in a Large Eddy Simulation (LES) approach. Whereas its original purpose was to provide sufficient algorithmic dissipation for a stable and convergent numerical method, more recently, it has been utilized as a subgrid-scale (SGS) model to account for the effect of small scales, unresolvable by the discretization. The freestream Mach number is 2.5, and direct comparison with a DNS database from our research group, as well as with experiments from the literature of adiabatic supersonic spatially turbulent boundary layers, is performed. Turbulent inflow conditions are generated via our dynamic rescaling-recycling approach, recently extended to high-speed flows. Focus is given to the assessment of the resolved Reynolds stresses. In addition, flow visualization is performed to obtain a much better insight into the physics of the flow. A weak compressibility effect is observed on thermal turbulent structures based on two-point correlations (IC vs. supersonic). The Reynolds analogy (u ' vs. t ') approximately holds for the supersonic regime, but to a lesser extent than previously observed in incompressible (IC) turbulent boundary layers, where temperature was assumed as a passive scalar. A much longer power law behavior of the mean streamwise velocity is computed in the outer region when compared to the log law at Mach 2.5. Implicit LES has shown very good performance in Mach 2.5 adiabatic flat plates in terms of the mean flow (i.e., C-f and U-VD(+)). iLES significantly overpredicts the peak values of u ', and consequently Reynolds shear stress peaks, in the buffer layer. However, excellent agreement between the turbulence intensities and Reynolds shear stresses is accomplished in the outer region by the present iLES with respect to the external DNS database at similar Reynolds numbers.
引用
收藏
页数:24
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