$FOAM_TUTORIALS/compressible/rhoCentralFoam/forwardStep

A virtual non-viscous gas flow, "normalized" to have a sound velocity of 1 m/s at a temperature of 1 K, hitting an obstacle at supersonic speed is calculated for 4 seconds.

The gas flows in from the region "inlet" at 3 m/s (Mach number 3) and out from the region "outlet". The region "top" and "bottom" are symmetric boundaries, and the region "obstacle" is a slip wall.

Model geometry

The turbulence model is not used, and the analysis is performed in 2-dimensions.

The physical properties of the gas are specified in the file constant/thermophysicalProperties as follows.

mixture { specie { nMoles 1; molWeight 11640.3; } thermodynamics { Cp 2.5; Hf 0; } transport { mu 0; Pr 1; } }

The meshes are as follows, and the number of mesh is 16128.

Meshes

The calculation result is as follows.

The flow velocity is as follows.

Flow velocity at 0.5 sec (U)

Flow velocity at 2.5 sec (U)

Flow velocity at 4 sec (U)

And the pressure is as follows.

Pressure at 0.5 sec (p)

Pressure at 2.5 sec (p)

Pressure at 4 sec (p)

Note that the upper region of the computational domain, "top", is a symmetric boundary.

cp -r $FOAM_TUTORIALS/compressible/rhoCentralFoam/forwardStep forwardStep

cd forwardStep

blockMesh

rhoCentralFoam

paraFoam

cd forwardStep

blockMesh

rhoCentralFoam

paraFoam

105.64 seconds *Single, Inter(R) Core(TM) i7-8700 CPU @ 3.20GHz 3.19GHz