[mesik]

Dear Members of this Forum,

we are currently preparing experiments with shock waves at our university. For this purpose, we want to use shock waves that are generated when air flows through a convergent-divergent nozzle (Laval nozzle) at supercritical conditions.

First, we created an analytical model of the nozzle in the EES program. Then we moved to Ansys, where we verify the behavior of our geometry in different operating conditions. Currently, we have created a fully functional CFD simulation that shows us what, for example, the mass flow through the nozzle will be at a given pressure at the inlet and outlet. However, manually changing conditions and rewriting data into a table is relatively time-consuming and inefficient, and since humans are lazy creatures, we naturally try to simplify and automate the work as much as possible.

My question is quite simple:

Is it possible to set the automatic change of boundary conditions in Fluent when the convergence of the simulation is reached?

Specifically, I have a certain inlet pressure of, for example, 700 kPa. The simulation will converge. The value of the mass flow, outlet velocity magnitude, and Mach number will be written to the table, file, or graph, and then the inlet pressure is automatically changed, for example to 600 kPa. The simulation will converge again, the values will be recorded and the whole process is repeated again. All this will be in the previously set range of the inlet pressure in the given step of pressure.

It will probably be some combination of a procedure and inserting data using a table in a .txt file. Unfortunately, I have no idea how to implement all this in Solver.

Thank you in advance for any advice.

Mesik