The archive consists of cases. Each case represents a geometric configuration and flow condition (i.e. ONERA M6 wing, MADIC 3D nozzle). A case can be classified as either a verification or validation case depending on whether the comparison data for the case is exact (analytical) or experimental, respectively. Each case contains one or more studies. Each study consists of one or more runs of the Wind-US code (or another CFD code). Throughout some of the cases and studies are detailed examples that provide a step-by-step description or tutorial on using WIND and associated tools.
Downloading Files from the Archive
The cases of the archive include:
Mach 7, Laminar 15-degree Ramp
Oblique shock on a 15 degree wedge at Mach 2.5
Conical shock on a 10 degree cone at Mach 2.35.
Prandtl-Meyer 15 Degree Expansion Corner at Mach 2.5.
Blasius Incompressible Laminar Flat Plate
Steady, Inviscid Flow in a Converging-Diverging Verfication (CDV) Nozzle.
Incompressible, Turbulent Flat Plate
Fraser Subsonic Conical Diffuser
Incompressible, Buice Axisymmetric Diffuser
Supersonic Axisymmetric "submerged" Jet Flow
Driver-Seegmiller Incompressible Backward-Facing Step
Sajben Transonic Converging-Diverging Diffuser
MADIC 2D Axisymmetric CD Boattail Nozzle
Hydrogen-Air Combustion in a Channel
Dual-Stream Hydrogen-Air Mixing
Laminar Flow over a Circular Cylinder