Allscale: Reference Data Of A Flow Over A Plane. Dpw-4 Performed With Fine/Open

The present computation has been performed on a 66 millions cells mesh. The turbulence model used is the Spalart Allmaras using CPU-Booster. Flow configuration : M = 0.85 Re = 5 000 000 AoA = 0.040472087 radians Integral results: CL = 0.49328 CD = 2.701862e-2 CM = -4.89841e-2 Geometry and refernce data can be found on the DPW-4 website : https://aiaa-dpw.larc.nasa.gov/Workshop4/DPW4-geom.html The data set provide one cgns file of the 3D mesh with the primitives variables in order to compare the reference application and the AllScale prototype.