I am trying to perform computational fluid dynamics on the compressible flow of a turbo compressor as shown below, but I get an error and cannot calculate.
Someone help
I get an error when I enter 0 pressure ”Floating point exception”
please have a look at this article about the issue.
I hope that helps. I also saw that you have a time depending table for your pressure outlet in a steady state simulation. What is the reason behind this?
Hi,
Can you try to change the pressure outlet boundary condition from a fixed value to a mean value.
With that the pressure at the outlet will be calculated accordingly to the flow situation.
One cause of floating point exception errors is a calculation that returns “Not a number”. One common occurrence is a division by zero (i.e. infinity).
By setting pressure to zero in a compressible simulation, you are getting exactly that: a division by zero in a calculation.
Are you sure that you need an absolute pressure of zero for a turbo compressor?