TY - GEN
T1 - Assessment and modification for Reynolds stress transport turbulence model flow
AU - Hajjawi, M.
AU - Taylor, L.
AU - Nichols, S.
PY - 2008
Y1 - 2008
N2 - The Launder-Shima1 Reynolds stress model is implemented in an existing scalable parallel flow solver. The complexity of the dissipation equation for this model adds stiffness and instability characteristics to the equation system, particularly when integrating to the wall with sub-layer resolution. In the present work, the dissipation equation from Launder-Shima model was replaced by the well known k-ε model dissipation equation in an effort to produce a more robust and stable Reynolds stress model. Computations for standard flat plate, square cylinder, backward facing step, surface mounted cube, and DARPA SUBOFF body are compared to experimental data for both models. The modified model showed a significant improvement in stability and robustness over the Launder-Shima model, while keeping the same flow prediction accuracy.
AB - The Launder-Shima1 Reynolds stress model is implemented in an existing scalable parallel flow solver. The complexity of the dissipation equation for this model adds stiffness and instability characteristics to the equation system, particularly when integrating to the wall with sub-layer resolution. In the present work, the dissipation equation from Launder-Shima model was replaced by the well known k-ε model dissipation equation in an effort to produce a more robust and stable Reynolds stress model. Computations for standard flat plate, square cylinder, backward facing step, surface mounted cube, and DARPA SUBOFF body are compared to experimental data for both models. The modified model showed a significant improvement in stability and robustness over the Launder-Shima model, while keeping the same flow prediction accuracy.
UR - https://www.scopus.com/pages/publications/77958508963
M3 - Conference contribution
AN - SCOPUS:77958508963
SN - 9781563479373
T3 - 46th AIAA Aerospace Sciences Meeting and Exhibit
BT - 46th AIAA Aerospace Sciences Meeting and Exhibit
T2 - 46th AIAA Aerospace Sciences Meeting and Exhibit
Y2 - 7 January 2008 through 10 January 2008
ER -