MODIFICATION OF THE SSG/LRR-ω RSM FOR ADVERSE PRESSURE GRADIENTS USING TURBULENT BOUNDARY LAYER EXPERIMENTS AT HIGH Re

A modification of the SSG/LRR-ω model for turbulent boundary layers in adverse pressure gradient is presented. The modification is based on a new wall law for the mean velocity at adverse pressure gradient. The wall law is found from two new joint DLR/UniBw experiments and from the analysis of a data base from the literature. The mean velocity profile in the inner layer is found to consist of a log-law region, which is thinner than its zero pressure gradient counterpart, and a half-power law region above the log law. An empirical correlation for the wall-distance of the transition from the log-law to the half-power law is presented. Then a modification of the ω-equation to account for a half-power law behaviour of the mean velocity is described. The modified SSG/LRR-ω model is then applied to the two joint DLR/UniBw experiments. The modification leads to a reduction of the mean velocity in the inner part of the boundary layer and makes the model more susceptible for flow separation, which is in good agreement with the experimental data.