Hello all!!
There is a fluid flow problem, the boundary conditions at the inlet are as follows: V= .1 m/sec, T=305 K, Pressure=1300000 pa. I am using the velocity inlet option. What value should I put in the Supersonic /initial Gauge Pressure tab? The default operating pressure is 101325 pa.
I am studying a fluid(Refrigerant) out from the condenser of an AC system, where the pressure is at 1320000 pa. This fluid (outlet from the condenser) is the inlet condition for my study.
Sir, with due respect, can anyone suggest to me how to implement this pressure into the fluent?
Because you have set the velocity boundary condition at the entrance, in this case you can set the pressure boundary condition at the exit, of course, you do not have the exit pressure of your system, which you have to calculate approximately. Of course, if the output of the condenser is the input of your system, and it returns to the condenser from your system (like a freezer circuit), you must calculate the increase in the pressure of the compressor and also the path loss.
- Badges
- Science topic
- Similar topics
- Physical Sciences
- Condensed Matter Physics
- Soft Matter
- Liquids