I was wondering at the steady state concept conventionally used in conventional grid based Eulerian techniques. Like cases such as Poiselluie flow where a fully flow developed profile is the steady state solution, temperature across a cantilever beam that has boundary conditions at both ends. I believe we iterate the solution until a steady state is achieved.
In contrast for a Lagrangian based SPH technique, I am little confused as to how to know if the flow has reached steady state or not. If I have a case of nozzle flow, with very high inlet pressure of about 300 MPa, so its becomes like a jet crusing through a nozzle and coming out of it with velocities close to 800-900 m/s, with the Reynolds number of this flow, I see turbulent boundary layer at the walls. So, coming to my question for such a case like this, how do I know if the flow in the nozzle has reached steady state or not? How do I decide when the flow is reaching equilibrium?
I am hoping to know if you all have some idea about this. It would help greatly. Thank you.
Siddharth