thrust of a nozzle
 

Hi,

I want to determine the thrust vector for a nozzle, with the strength menu, i can find the center of pressure but i don't know if it's possible to have the coordinates of the thrust vector...

Also, i wonder if for model a nozzle (with Mach max is near 4) it's better to use Density based or Pressure based, with P-B i have results more logical in the determination of center of pressure (The velocity is very high only in the divergent of the nozzle)...

Can you help me,

Thanks,