Any help would be hugely appreciated on this confusing issue.
I'm modelling an external supersonic flow of M=2 around an aircraft. The boundary conditions are a pressure far field.
Using the isentropic flow relations, for my altitude (18,300m) the static pressure is 7,158 Pa, which using the isentropic flow relations gives a total pressure as 56,008 pa. I input this as the gauge pressure in the far field boundary condition.
Operating pressure is set to zero.
I set the simulation to provide me with dynamic pressure as I need to calculate a drag coefficient, however upon viewing it in Post, the dynamic pressure in the far field is ~3x higher than the total pressure I input??
Is there something I'm missing here? I've gone over my setup over and over and it seems fine.
Thanks very much in advance.