An eddy-viscosity subgrid-scale model for turbulent shear flow: Algebraic theory and applications

By A. W. Vreman. 2004

1,312 citations recorded by the source corpus.

Subfields: Biomedical Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/302016ad6208e70bac1e87ca8dbe95251a75c4ab

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In Biomedical Engineering

In Computational Mechanics

Citations in the corpus

Importance of the nozzle-exit boundary-layer state in subsonic turbulent jets (2018, methodology): “The Vreman (2004) subgrid model is used to account for the physical effects of unresolved turbulence on the resolved flow, with constant coefficient set to the recommended value of c = 0.07.”
Confinement effects in shock wave/turbulent boundary layer interactions through wall-modelled large-eddy simulations (2014, methodology): “Subgrid-scale stresses are explicitly modelled following Vreman (2004), and a fixed turbulent Prandtl number of 0.9 is used to model the subgrid-scale heat flux.”
Fire dynamics simulator technical reference guide volume 1 :: mathematical model (2013, methodology): “4 Vreman’s Model Vreman’s eddy viscosity model [31] is given by”
Unsupervised deep learning for super-resolution reconstruction of turbulence (2020, methodology): “Our CycleGAN was trained and tested using the input LES data obtained by the Vreman subgrid-scale model.”
Resolvent-analysis-based design of airfoil separation control (2018, methodology): “Vremen’s sub-grid scale model (Vreman 2004) is utilized in the LES.”
A new hybrid recursive regularised Bhatnagar–Gross–Krook collision model for Lattice Boltzmann method-based large eddy simulation (2018, methodology): “It is important noting that ILES based on the dynamic HRR-BGK is not strictly equivalent to a classical BGK coupled to theVreman’smodel, since the scale-byscale distributions of the total dissipation are not equivalent.”
Wavepacket models for supersonic jet noise (2014, methodology): “The Vreman subgrid-scale model (Vreman 2004; You & Moin 2007) is used with constant coefficients (c= 0.07, Prt = 0.9) to account for the physical effects of the unresolved turbulence on the resolved flow.”
Exponential roughness layer and analytical model for turbulent boundary layer flow over rectangular-prism roughness elements (2016, methodology): “Simulation set-up We use the in-house finite-difference code Vicar3D to solve the incompressible filtered Navier–Stokes equations, including the Vreman subgrid-scale model (Vreman 2004; You & Moin 2007) and the iWMLES model for the near-wall closure (Yang et al. 2015).”
Large Eddy Simulations of gaseous flames in gas turbine combustion chambers (2012, neutral): “Vreman [98] Production 1⁄4 dissipation O(y(1)) z0:71 0 z1:22 1”