$FOAM_TUTORIALS/compressible/rhoCentralFoam/obliqueShock

A virtual non-viscous gas flow, "normalized" to have a sound velocity of 1 m/s at a temperature of 1 K, flowing in from two directions and colliding each other, is calculated for 10 seconds.

The gas flows in from the region "inlet" at 2.9 m/s (Mach number 2.9) and the region "top" at (2.61933, -0.50632) m/s (Mach number about 2.66), and after colliding, flows out from the region "outlet". The region "bottom" is set to a symmetric boundary.

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 1800.

Meshes

The calculation result is as follows.

The flow velocity is as follows.

Flow velocity at 1 sec (U)

Flow velocity at 2 sec (U)

Flow velocity at 10 sec (U)

And the pressure is as follows.

Pressure at 1 sec (p)

Pressure at 2 sec (p)

Pressure at 10 sec (p)

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

cd obliqueShock

blockMesh

rhoCentralFoam

paraFoam

cd obliqueShock

blockMesh

rhoCentralFoam

paraFoam

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