Compressible

Find projects using the compressible analysis type here. | Page 194

Studying compressible and incompressible flow around a wing and changes of angle of attack.

analysis of micro stream by surface tension

Characterisation of the pressure drop over a gantry

Finally characterising the pressure drop for the new design

Just a sim on the batman wing to see how it would work.

The inlet Mach number is 3, and the wedge angle is 20 degrees. In this validation case, we also compare the dependence of the solution on the mesh resolution.  We also show two methods to capture the shock wave, namely, numerical Schlieren (gradient of density), and numerical shadowgraph (Laplacian of the gradient).

Model rocket designed to run 29mm diameter motors

To determine the CFD of the aircraft's wings

Turbulence Test: Under Water: 4Px 1Py 8Pz Single Periodical Pillar Jet

Velocity Body:  X, Y, Z, All XYZ. 
Velocity Nodes:  X, Y, Z, All XYZ.

Compressible | SimScale Project Library | Page 194