Compressible

Find projects using the compressible analysis type here. | Page 190

Simulation of Max Q for F9 Rocket model. Project for University

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).

Seeing if pushing out some air in front (like a retropropulsion rocket, but not supersonic) will decrease or increase the drag of a supersonic object

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

Almost all the necessary tests are completed. Tested in ALL XYZ, X, Y , Z. There are preparation stages in previous tests. At the same time previous test results (Tests: 3, 4, 5, 6, 7_1) are not bad.

Campo de velocidad y distribución de presiones para flujo en un escalón

Campo de velocidad y distribución de presión para flujo en un escalón

demonstrar o escoamanto do ar na asa de um aviao