LES of canonical shock-turbulence interaction
نویسنده
چکیده
The interaction between shock waves and turbulence is present in a large variety of high-speed flows with relevance in scientific and engineering applications. The use of largeeddy simulations (LES) to predict such flows requires subgrid-scale (SGS) models capable of accurately representing the physics behind this interaction at the unresolved scales. The canonical shock-turbulence interaction problem, consisting of isotropic turbulence passing through a nominally normal shock, isolates the fundamentals of this mutual interaction and can be considered a good benchmark case to test the performance of SGS models. The problem of shock-turbulence interaction has been studied theoretically (Ribner 1953; Lee et al. 1992; Lele 1992; Jacquin et al. 1993; Wouchuk et al. 2009), experimentally (Hesselink & Sturtevant 1988; Keller & Merzkirch 1990; Barre et al. 1996; Agui et al. 2005) and numerically, both through direct numerical simulations (DNS) (Lee et al. 1993, 1997; Hannappel & Friedrich 1995; Mahesh et al. 1997; Larsson & Lele 2009) and LES (Lee 1992; Ducros et al. 1999). LES of the canonical case are nonetheless scarce in the literature, compared, for example, with LES of the shock-boundary layer interaction. The aim of the present work is to compare the performance of several SGS models for LES of the canonical shock-turbulence interaction problem, focusing on the region immediately downstream of the shock, which poses most of the modeling challenges (BermejoMoreno 2009). DNS results obtained following Larsson & Lele (2009) will be used for comparison. Section 2 describes the mathematical formulation, geometric configuration and numerical method used in this study. The SGS models implemented for comparison are introduced in Section 3. We propose in Section 4 a conditional application of the SGS model that avoids adding SGS dissipation to flow regions where excessive numerical dissipation is expected. LES results are presented in Section 5 for different flow conditions and compared with filtered DNS data, also evaluating the influence of the grid resolution, numerical scheme and conditional SGS application. Conclusions and future plans are presented in Section 6.
منابع مشابه
Study of Parameters Affecting Separation Bubble Size in High Speed Flows using k-ω Turbulence Model
Shock waves generated at different parts of vehicle interact with the boundary layer over the surface at high Mach flows. The adverse pressure gradient across strong shock wave causes the flow to separate and peak loads are generated at separation and reattachment points. The size of separation bubble in the shock boundary layer interaction flows depends on various parameters. Reynolds-averaged...
متن کاملResolution and Energy Dissipation Characteristics of Implicit LES and Explicit Filtering Models for Compressible Turbulence
Solving two-dimensional compressible turbulence problems up to a resolution of 16, 3842, this paper investigates the characteristics of two promising computational approaches: (i) an implicit or numerical large eddy simulation (ILES) framework using an upwind-biased fifth-order weighted essentially non-oscillatory (WENO) reconstruction algorithm equipped with several Riemann solvers, and (ii) a...
متن کاملA Study of Supersonic Compression-Corner Interactions using Hybrid LES/RANS Models
Number of Papers published in peer-reviewed journals: Number of Papers published in non peer-reviewed journals: A Study of Supersonic Compression-Corner Interactions using Hybrid LES/RANS Models Report Title This research has developed a new hybrid large-eddy /Reynolds-averaged Navier-Stokes turbulence closure strategy specifically designed for strongly interacting, wall-bounded flows. The mode...
متن کاملLES Study on Mechanism of Reduction of Shock Induced Flow Separation by MVG
Shock-boundary layer interaction (SBLI) is a kind of problem which is frequently met in supersonic engine inlet flow and external flow. A detail study on mechanism of reduction of shock induced flow separation by MVG is carried out by high order implicit large eddy simulation (LES). To generate the fully developed turbulent flow, a series of turbulent profiles are given by previous DNS simulati...
متن کاملTurbulence structure behind the shock in canonical shock–vortical turbulence interaction
The interaction between vortical isotropic turbulence (IT) and a normal shock wave is studied using direct numerical simulation (DNS) and linear interaction analysis (LIA). In previous studies, agreement between the simulation results and the LIA predictions has been limited and, thus, the significance of LIA has been underestimated. In this paper, we present high-resolution simulations which a...
متن کامل