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Data-driven Reynolds stress models based on the frozen treatment of Reynolds stress tensor and Reynolds force vector

Physics of Fluids, 2023
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.
Ali Amarloo   +4 more
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Modeling of the Reynolds Stress Transport Equation

AIAA Journal, 1997
An empirical strategy for improving modeling of the energy dissipation rate e ij and the velocity-pressure gradient Π 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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Differential Reynolds-Stress Modeling for Aeronautics

AIAA Journal, 2015
A comparison of two differential Reynolds-stress models for aeronautical flows is presented. The ω model herein combines the Speziale–Sarkar–Gatski pressure–strain model with the Launder–Reece–Rodi model toward the wall, where the length scale is supplied by Menter’s baseline ω equation.
Cécora, René-Daniel   +3 more
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Reynolds-stress-transport modeling for compressible aerodynamics applications

AIAA Journal, 1999
Progress is reported in the development of a nonlinear Reynolds-stress-transport model for compressible, turbulent flow. The focus is on a variation of a particular cublc model that does not require the usual topography-related parameters, such as normal-to-wall vectors.
P. Batten   +3 more
openaire   +1 more source

Reynolds stress model involving the mean spin tensor

Physical Review E, 2004
In this work, we develop a Reynolds stress model along the line of the approach presented by Commun. Nonlinear Sci. Numer. Simul. 9, 543 (2004)]], aiming to assess the role and contribution of the mean spin tensor in turbulence modeling. Here, the constitutive functional for the Reynolds stress depends on the mean spin tensor as well as the mean ...
Yu-Ning, Huang, Hui-Yang, Ma
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Model functions of Reynolds stress models

The Physics of Fluids, 1988
A Reynolds stress (Re-stress) model for the prediction of shear flows is presented. Special attention is paid to the determination of the model functions. First, the general modeling assumptions are discussed and the modeling of the equations is then described in detail. It is shown that by successive analysis of different types of flows a set of model
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Reynolds Stress Models for Shock-Turbulence Interaction

2019
A systematic deficiency of current turbulence models which are based on the Reynolds-averaged Navier-Stokes equations (RANS) is their inability to correctly predict the interaction of turbulence with shocks. This is because RANS models do not account for the unsteady motion or fragmentation of the shock wave within the interaction zone.
Karl, Sebastian   +2 more
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Reynolds-stress modelling of transonic afterbody flows

The Aeronautical Journal, 2001
AbstractSeveral afterbody flows, involving shock-boundary-layer interaction, are used to evaluate recent developments in a realizable low-Reynolds-number, second-moment closure of turbulence. The model considered is a compressibility-adapted variant of the recent incompressible-flow form of Craft and Launder. This includes a tensorially cubic model for
M. A. Leschziner, P. Batten, T. J. Craft
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Dynamic Reynolds stress modeling of turbidity currents

Journal of Geophysical Research: Oceans, 1992
A turbidity current is idealized as a time‐varying, one‐dimensional boundary layer flow. A full Reynolds stress model appears to give significantly better predictions than one‐ and two‐equation turbulence closures. Model verification is obtained from stationary downslope experimental flows.
Bård Brørs, Karl J. Eidsvik
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Reynolds Stress Modeling for Hypersonic Flows

2012
Despite 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].
A. Bosco   +4 more
openaire   +1 more source

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