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55th AIAA Aerospace Sciences Meeting
Full seven-equation Reynolds stress turbulence models are promising tools for today's aerospace technology challenges. This paper examines two such models for computing challenging turbulent flows including shock-wave boundary layer interactions, separation and mixing layers. The Wilcox and the SSG/LRR full second-moment Reynolds stress models have been implemented into the FUN3D unstructured Navier-Stokes code and were evaluated for four problems: a transonic two-dimensional diffuser, adoi:10.2514/6.2017-0541 fatcat:fs473ymvbrablp46kbtt2gygj4