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Reynolds-Stress Model for Eulerian multiphase
Progress in Computational Fluid Dynamics, 2006Summary: This paper presents a way of modelling turbulence in multiphase flows within the context of the Reynolds-Stress Model. The model has been implemented in the general-purpose unstructured finite volume code Fluent V6. Two multiphase turbulence approaches were considered: mixture and dispersed models.
Giuseppina Montante
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A Reynolds-Stress Model for Near-Wall and Low-Reynolds-Number Regions
Journal of Fluids Engineering, Transactions of the ASME, 1988The Reynolds stress model for high Reynolds numbers proposed by Launder et al. is extended to near-wall and low-Reynolds-number regions. In the development of the model, particular attention is given to the high anisotropy of turbulent stresses in the immediate vicinity of a wall and to the behavior of the exact stress equation at the wall. A transport
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An improved algebraic Reynolds stress model and corresponding nonlinear stress model
Physics of Fluids A, Fluid Dynamics, 1992An improved algebraic Reynolds stress model is developed from the modeled dynamic equations for the Reynolds stress. The improved model more closely represents the original Reynolds stress model equation than the standard algebraic Reynolds stress model over the range of time scales for the turbulence and mean flow strain field.
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For developing a reliable data-driven Reynold stress tensor (RST) model, successful reconstruction of the mean velocity field based on high-fidelity information (i.e., direct numerical simulations or large-eddy simulations) is crucial and challenging, considering the ill-conditioning problem of Reynolds-averaged Navier–Stokes (RANS) equations.
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Modeling of the Reynolds Stress Transport Equation
AIAA Journal, 1997An empirical strategy for improving modeling of the energy dissipation rate e ij and the velocity-pressure gradient Î ij terms in the transport equations for the Reynolds stresses is proposed on the basis of available direct numerical simulations of the turbulent boundary layer and fully developed turbulent channel flow.
Djenidi, L., Antonia, R. A.
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Reynolds Stress Modeling for Hypersonic Flows
2012Despite the enormous increase in computational capabilities and use of computational fluid dynamics as a design tool in the aircraft industry, the correct prediction of complex hypersonic turbulent flows involving shock wave boundary layer interaction (SWBLI) is still a challenge [1].
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