scispace - formally typeset
Open Access

Improved two-equation k-omega turbulence models for aerodynamic flows

Florian R. Menter
- Vol. 93, pp 22809
Reads0
Chats0
TLDR
In this article, two new versions of the k-omega two-equation turbulence model are presented, the baseline model and the Shear-Stress Transport model, which is based on the BSL model, but has the additional ability to account for the transport of the principal shear stress in adverse pressure gradient boundary layers.
Abstract
Two new versions of the k-omega two-equation turbulence model will be presented. The new Baseline (BSL) model is designed to give results similar to those of the original k-omega model of Wilcox, but without its strong dependency on arbitrary freestream values. The BSL model is identical to the Wilcox model in the inner 50 percent of the boundary-layer but changes gradually to the high Reynolds number Jones-Launder k-epsilon model (in a k-omega formulation) towards the boundary-layer edge. The new model is also virtually identical to the Jones-Lauder model for free shear layers. The second version of the model is called Shear-Stress Transport (SST) model. It is based on the BSL model, but has the additional ability to account for the transport of the principal shear stress in adverse pressure gradient boundary-layers. The model is based on Bradshaw's assumption that the principal shear stress is proportional to the turbulent kinetic energy, which is introduced into the definition of the eddy-viscosity. Both models are tested for a large number of different flowfields. The results of the BSL model are similar to those of the original k-omega model, but without the undesirable freestream dependency. The predictions of the SST model are also independent of the freestream values and show excellent agreement with experimental data for adverse pressure gradient boundary-layer flows.

read more

Content maybe subject to copyright    Report

Citations
More filters
Journal ArticleDOI

Film-cooling Performance in Supersonic Flows: Effect of Shock Impingement

TL;DR: In this article, high pressure turbine stages work in transonic regimes and then shock waves, shed by the trailing edge, impinge on the suction side modifying the flow structures. Gas turbine entry temperature is m...
Journal ArticleDOI

Near-wall grid adaptation for turbulent flows

TL;DR: Grid-adaptation techniques for the boundary-layer region of hybrid meshes, where the mesh is of regular structure consisting of prismatic respectively hexahedral elements, are considered to improve convergence, accuracy and reliability of aerodynamic simulations for viscous flows.

Model-consistent universal wall-functions for RANS turbulence modelling

TL;DR: In this paper, a model-consistent universal wall function method for RANS turbulence modelling is presented, which gives solutions almost independent of the position of the first grid node above the wall and allows a considerable solver acceleration and reduction of memory consumptions.
DissertationDOI

Computational and Experimental Comparison of a Powered Lift, Upper Surface Blowing Configuration

TL;DR: In this paper, the use of CFD as a validation tool for wind tunnel data on 2D high lift airfoil with a 3D engine performed by Georgia Tech Research Institute was demonstrated.
References
More filters