[monigabriela6]

Hello everyone,

I am trying to produce a CFD simulation on an axial fan so that I can analyse the air flow and power produced against the static pressure. So far I have managed to produce the enclosure and the rotating body and I am trying to prepare the setup for the simulation.

For the boundary conditions I am using velocity inlet and pressure outlet. I have tried to assign different values for the velocity so that I can get different values of the air flow. I am getting the value of the air flow by using reports section and then go to fluxes and check the mass flow rate and multiply it by the density value. However, I don't know how to check the Static pressure value for this air flow. Can someone help me with this please?

[CFD-fellow]

report>surface integrals>mass weighted average>static pressure@inlet