Dynamic wall modeling for large-eddy simulation of complex turbulent flows

By Meng Wang, Parviz Moin. 2002

441 citations recorded by the source corpus.

Subfields: Computational Mechanics, Environmental Engineering

View Paper: https://www.semanticscholar.org/paper/edaa62911f5d8f5df57f637a7530875045854bd3

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Computational Mechanics

1. Sanjiva K. Lele
2. Johan Larsson
3. Soshi Kawai
4. Tim Colonius
5. F. Menter
6. Lars Davidson
7. P. Spalart
8. Meng Wang

In Environmental Engineering

1. Sanjiva K. Lele
2. F. Menter
3. Lars Davidson
4. Johan Larsson
5. Tim Colonius
6. Soshi Kawai
7. Meng Wang
8. P. Spalart

Citations in the corpus

• COMPUTATIONAL PREDICTION OF FLOW-GENERATED SOUND (2006, methodology): “If part of the Reynolds stress is represented in the wall model equations, the RANS eddy viscosity needs to be reduced to match the total stress at the RANS/LES interface (Cabot & Moin 2000, Wang & Moin 2002).”
• Wall-layer models for large-eddy simulations (2008, methodology): “Wang [10].”
• Development of DDES and IDDES Formulations for the k-ω Shear Stress Transport Model (2012, methodology): “In addition, wellresolved LES (Wang and Moin [21, 22]) and experimental data [20] are included.”
• The inner–outer layer interface in large-eddy simulations with wall-layer models (2003, positive): “This method has been used in channel flow at high Reynolds numbers (Balaras et al., 1996), backwardfacing steps (Cabot, 1996; Diurno et al., 2001), and in calculations of the trailing edge of an airfoil (Wang and Moin, 2002), with fairly accurate results.”
• Large eddy simulation with modeled wall-stress: recent progress and future directions (2016, methodology): “…in the literature has been to simply discard the convective terms (i.e., ∂(uu j)/∂x j) while retaining the pressure-gradient term and, in some cases, the time-derivative term as well (Hoffmann & Benocci, 1995; Wang & Moin, 2002; Catalano et al., 2003; Duprat et al., 2011; Chen et al., 2014).”
• A hybrid RANS-LES approach with delayed-DES and wall-modelled LES capabilities (2008, result): “15 compares results of the present simulation with: the experimental data; the wall-resolved LES of Wang and Moin (2002) carried out with the use of the dynamic SGS model on a C-grid with nearly 7 million nodes; and the hybrid LES-RANS model of Tessicini et al. (2006) with prescribed RANSLES…”
• Turbulent Wall Model for Immersed Boundary Methods (2011, methodology): “(12) is proposed in [31], where the model is coupled with an incompressible LES method.”
• Wall-modeling in large eddy simulation: Length scales, grid resolution, and accuracy (2012, background): “The basic reasoning holds for a wide range of wall-stress models, including equilibrium models (e.g., the famous log-law) and more elaborate approaches that solve the thin boundary layer equations on an auxliary grid near the wall (cf. Cabot & Moin 1999; Wang & Moin 2002; Kawai & Larsson 2010).”
• Large-eddy simulation and wall modelling of turbulent channel flow (2009, methodology): “Instead of the log law, the thin boundary layer equations (TBLEs) coupled with a damped mixinglength eddy viscosity can also be used, giving good agreement with experiments even in separating flows (Cabot & Moin 1999; Wang & Moin 2002).”
• Large Eddy Simulations: How to evaluate resolution (2009, methodology): “Another way to model the near-wall region is to use two-layer models (Balaras et al., 1996; Cabot, 1995; Cabot and Moin, 1999; Wang and Moin, 2002), also called “thin boundary layer equations”.”
• Confinement effects in shock wave/turbulent boundary layer interactions through wall-modelled large-eddy simulations (2014, background): “…complete, wall-model formulations that do not assume equilibrium have been proposed in the literature (see, e.g., Cabot 1995; Balaras, Benocci & Piomelli 1996; Wang & Moin 2002; Kawai & Larsson 2013), by retaining one or multiple of the additional terms neglected under the equilibrium assumption.”
• Aerodynamics of Heavy Vehicles (2014, methodology): “…promising WMLES approach is to perform LES with the wall shear stress as the boundary condition at the wall (instead of the no-slip condition) without resolving the near-wall region (Chung & Pullin 2009, Kawai & Larsson 2012, Lee et al. 2013, Nicoud et al. 2001, Schumann 1975, Wang & Moin 2002).”