## Supersonic Turbulent Flow Past a Prism

## Supersonic Turbulent Flow Past a Prism

This tutorial example sets up and solves supersonic compressible flow around a triangular prism, with viscous effects and turbulence using the OpenFOAM solver.

The inflow is supersonic at 650 m/s causing shock waves to form when the flow field impacts the prism, and also secondary waves following the trailing edges and …

## Supersonic Flow Past a Wedge

## Supersonic Flow Past a Wedge

This verification test case studies steady inviscid compressible flow past a
wedge at an incident angle of 15 degrees. As the supersonic flow (*Ma = 2.5*)
hits the wedge a sharp oblique shock wave is formed, resulting in a reduced
downstream flow velocity. The simulation uses the inviscid compressible Euler
equations to …

## Supersonic Flow Over an Obstacle

## Supersonic Flow Over an Obstacle

Steady inviscid flow over a cylindrical bump using the compressible
Euler equations. The flow at the inlet is supersonic with *Ma = 1.4*
resulting in a series of reflected shock waves as the flow hits the
obstacle]. The obstacle could represent anything from a protrusion on
an aircraft wing to a structural feature in a …