This paper deals with the three-dimensional RANS computations of the transonic flow around the DLR-F4 wing-body configuration with a wall law approach. A study of the behaviour of different transport-equation turbulence models is given with comparisons to experimental data. The structure of the three-dimensional flow separation predicted by the computations is described and its topological coherence is checked. Moreover, to drastically reduce the CPU cost, a computation with a multigrid method coupled to wall functions has been tested.
Numerical Simulation of the DLR-F4 Wing/Body Configuration With Wall Functions
- Views Icon Views
- Share Icon Share
- Search Site
Goncalves, E, & Houdeville, R. "Numerical Simulation of the DLR-F4 Wing/Body Configuration With Wall Functions." Proceedings of the ASME 2002 Joint U.S.-European Fluids Engineering Division Conference. Volume 1: Fora, Parts A and B. Montreal, Quebec, Canada. July 14–18, 2002. pp. 1267-1274. ASME. https://doi.org/10.1115/FEDSM2002-31097
Download citation file: