Results 261 to 270 of about 58,998 (325)

The Anisotropic Hybrid k-$$\omega $$ SST/Stochastic Turbulence Model

open access: closed, 2020
This chapter focuses on a brief summary of the mathematical formulation of the anisotropic hybrid k-\(\omega \) Shear-Stress Transport (SST)/Stochastic Turbulence Model (STM) related to a new hypothesis on the Reynolds stress tensor (2.41) proposed in the first volume of this book [17]. The mathematical formulation of the anisotropic hybrid k-\(\omega \
László Könözsy
semanticscholar   +3 more sources

A Three Equation Curvature and Rotation Sensitive Variant of the SST K-Omega Turbulence Model

open access: closedASME 2010 3rd Joint US-European Fluids Engineering Summer Meeting: Volume 1, Symposia – Parts A, B, and C, 2010
To date, eddy viscosity models are the most accepted and widely used RANS-based turbulence closures, attributable to their computational efficiency and relative robustness. One notable shortcoming of these models is their insensitivity to system rotation and streamline curvature.
Tej Prasad Dhakal, D. Keith Walters
semanticscholar   +3 more sources

Tuning of Generalized K-Omega Turbulence Model by Using Adjoint Optimization and Machine Learning for Gas Turbine Combustor Applications

open access: closedVolume 3B: Combustion, Fuels, and Emissions, 2023
For swirl-stabilized gas turbine combustors, turbulence modelling is generally undertaken using Scale-Resolved Simulations (SRS) methods such as Large Eddy Simulations (LES).
George Klavaris   +5 more
semanticscholar   +3 more sources

Stress Limiter Consideration for k-omega Turbulence Models in Shock-Wave/Turbulent Boundary-Layer Interactions in Supersonic and Hypersonic Flows

open access: closed20th AIAA Computational Fluid Dynamics Conference, 2011
The shear stress transport (SST) turbulence model of Menter was proposed to predict an accurate separated flow in the adverse pressure gradient flows, but it has sometimes failed to predict the flowfield with strong shock wave/turbulent boundary-layer interaction. In an effort to improve the original k-ω model, Wilcox has recently proposed a modified k-
Tan Jie, Jin Jie
semanticscholar   +3 more sources

Formulation of the k-omega Turbulence Model Revisited

45th AIAA Aerospace Sciences Meeting and Exhibit, 2007
This paper presents a reformulated version of the author'sk-ω model of turbulence. Revisions include the addition of just one new closure coefficient and an adjustment to the dependence of eddy viscosity on turbulence properties. The result is a significantly improved model that applies to both boundary layers and free shear flows and that has very ...
D. Wilcox
openaire   +2 more sources

Staggered finite volume scheme for solving cascade flow with a k-omega turbulence model

AIAA Journal, 1994
A k-ω turbulence model by Wilcox is applied to cascade flow calculations. A staggered finite volume scheme is proposed to solve the compressible Reynolds-averaged Navier-Stokes equations and the k-ω equations are solved on staggered control volumes with k and ω defined at the cell vertices of the original grid.
Liu, Fieng, Zheng, Xiaoqing
openaire   +2 more sources

Modification to the k-Omega Turbulence Model for Vortically Dominated Flows

open access: closed49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2011
[Abstract] Vortically dominated flows (wingtip, vortex-fin interaction, jet into cross-flow) have traditionally been difficult to accurately model using two-equation RANS (Reynolds Averaged NavierStokes) CFD tools. However RANS models provide the “workhorse” for many aerodynamic simulations.
Lawrence Dechant
openaire   +2 more sources

Application of the k-omega turbulence model to quasi-three-dimensional turbomachinary flows

open access: closedJournal of Propulsion and Power, 1996
Many computational fluid dynamics codes for turbomachinery use the Baldwin-Lomax (B-L) turbulence model. It is easy to implement in two dimensions and works well for predicting overall turbomachinery performance. However, it is awkward to implement in three dimensions, often has difficulty finding the length scale, has a crude transition model, and ...
Rodrick V. Chima
openaire   +2 more sources

Extension of the k-omega-SST turbulence model for flows over rough surfaces

open access: closed22nd Atmospheric Flight Mechanics Conference, 1997
This paper introduces an improved computational method for predicting the behaviour of turbulent flows over rough surfaces. The method is based on the numerical solution of the Navier-Stokes equations employing the k - w-SST turbulence model. An existing surface-roughness method, developed for the traditional k — w models, was found to not work well ...
Antti Hellsten   +3 more
openaire   +2 more sources

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