@article{thompson_hassan_2015, title={Simulation of a Variety of Wings Using a Reynolds Stress Model}, volume={52}, ISSN={["1533-3868"]}, DOI={10.2514/1.c033046}, abstractNote={The Wilcox 2006 stress-ω model, a Reynolds stress model, implemented in both the NASA Langley codes FUN3D and CFL3D, has been used to study a number of 2-D and 3-D cases. This study continues the assessments of the stress-ω model by simulating the flow over two wings: the DPW-W1 and the DLR-F11 wings. Using FUN3D, which uses unstructured grids, and CFL3D, which uses structured grids, the results were compared to solvers employing one- and two-equation turbulence models and experimental data. In general, in situations where experimental data is available, the stress-ω model performs as well or better than one- and two-equation models.}, number={5}, journal={JOURNAL OF AIRCRAFT}, author={Thompson, K. B. and Hassan, H. A.}, year={2015}, pages={1668–1680} }