![]() ![]() ![]() Results using using SA, SST, and EASM-ko turbulence models Subsonic flow past a semi-infinite flat plate is modeled at Reynolds numberīy specifying total pressure, total temperature, and Mach number. Note that the files for the 3D cases can be quite large. ![]() ![]() (steady demonstration of CGNS capability)Īll test cases are available for downloading as Unix compressed tarįiles containing grid, input, and auxiliary files. (demonstration of curvature correction model SARC) (unsteady demonstration of flow control through time-dependent BCs) (unsteady demonstration of sliding patched interface capability) (unsteady demonstration of moving grid capability) (steady demonstration of spatial accuracy) (unsteady demonstration of temporal accuracy) (steady derivatives with respect to alpha) Flat Plate with Grid Skew Effect (steady ĭemonstration of effect of different minimum wall spacing).
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