Extension of an amplification factor transport transitional approach with a reynolds stress model
Extension of an amplification factor transport transitional approach with a reynolds stress model
An extension of the amplification factor transport (AFT) transitional approach is presented with a SSG-LRR-ω Reynolds Stress Model (RSM). Exact descriptions of the convection and production terms for each Reynolds stress component and the pressure-strain by the RSM improve the description of the flow-field in near-wall region and the aft-part of the cylinder compared to linear-eddy-viscosity models (EVM). The implementation of the combined AFT19-RSM model is discussed and verified for different grid resolutions for a zero-pressure-gradient (ZPG) flat-plate. An enhanced anisotropic description of the Reynolds stress tensor in the near-wall region is predicted by the AFT19-RSM compared to Boussinesq-hypothesis closure. As an application of the model proposed in this paper, a two-dimensional (2D) analysis is performed for flow around a circular cylinder at four Reynolds numbers, in regimes covering the subcritical to the trans-critical regime. Results demonstrate an improved prediction within the wake of the cylinder compared to experimental data. Consequently, the better description of the wake improves the tendency of the CD estimation in the super-critical regime where there are two laminar separation bubbles on each side of the cylinder. The trans-critical prediction show that none of the transitional models tested, including the one proposed in this paper, can recover the fully-turbulent behaviour on the upstream face. This requires further investigation. The incorporation of the transitional framework to a RSM provides the capability of describing a laminar region, laminar separation, laminar separation bubble and turbulent reattachment. In addition, there is a slightly improved description of the flow on the downstream face of the cylinder compared to a more conventional Eddy Viscosity Model (EVM) approach.
American Institute of Aeronautics and Astronautics
Fernandez, Jose M.Garro
13e54601-9141-4bb1-9962-c4889a3434af
Angland, David
b86880c6-31fa-452b-ada8-4bbd83cda47f
Hu, Zhiwei
dd985844-1e6b-44ba-9e1d-fa57c6c88d65
19 June 2020
Fernandez, Jose M.Garro
13e54601-9141-4bb1-9962-c4889a3434af
Angland, David
b86880c6-31fa-452b-ada8-4bbd83cda47f
Hu, Zhiwei
dd985844-1e6b-44ba-9e1d-fa57c6c88d65
Fernandez, Jose M.Garro, Angland, David and Hu, Zhiwei
(2020)
Extension of an amplification factor transport transitional approach with a reynolds stress model.
In AIAA AVIATION 2020 FORUM.
vol. 1 PartF,
American Institute of Aeronautics and Astronautics..
(doi:10.2514/6.2020-2979).
Record type:
Conference or Workshop Item
(Paper)
Abstract
An extension of the amplification factor transport (AFT) transitional approach is presented with a SSG-LRR-ω Reynolds Stress Model (RSM). Exact descriptions of the convection and production terms for each Reynolds stress component and the pressure-strain by the RSM improve the description of the flow-field in near-wall region and the aft-part of the cylinder compared to linear-eddy-viscosity models (EVM). The implementation of the combined AFT19-RSM model is discussed and verified for different grid resolutions for a zero-pressure-gradient (ZPG) flat-plate. An enhanced anisotropic description of the Reynolds stress tensor in the near-wall region is predicted by the AFT19-RSM compared to Boussinesq-hypothesis closure. As an application of the model proposed in this paper, a two-dimensional (2D) analysis is performed for flow around a circular cylinder at four Reynolds numbers, in regimes covering the subcritical to the trans-critical regime. Results demonstrate an improved prediction within the wake of the cylinder compared to experimental data. Consequently, the better description of the wake improves the tendency of the CD estimation in the super-critical regime where there are two laminar separation bubbles on each side of the cylinder. The trans-critical prediction show that none of the transitional models tested, including the one proposed in this paper, can recover the fully-turbulent behaviour on the upstream face. This requires further investigation. The incorporation of the transitional framework to a RSM provides the capability of describing a laminar region, laminar separation, laminar separation bubble and turbulent reattachment. In addition, there is a slightly improved description of the flow on the downstream face of the cylinder compared to a more conventional Eddy Viscosity Model (EVM) approach.
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Published date: 19 June 2020
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AIAA AVIATION 2020 FORUM, , Virtual, Online, 2020-06-15 - 2020-06-19
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Local EPrints ID: 509760
URI: http://eprints.soton.ac.uk/id/eprint/509760
PURE UUID: 367f88d8-053c-4d3a-b808-8bb65758a8fa
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Date deposited: 04 Mar 2026 17:46
Last modified: 05 Mar 2026 02:38
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Author:
Jose M.Garro Fernandez
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