Hey, iam Simulation the flow in an axial turbine. The flow comes from the rotational detonation combustion, where 2 shockwaves travels around the annulus in the turbine. I just simulate 15 stator blades without rotor blades, so there is no rotation speed. At the Inlet of my domain for my unsteady Simulation I have the unsteady inlet boundary conditions where the total pressure and total temperature are functions of the time and the azimuthal angle. So in FINE/Open-Tutorial OpenLabs Tutorial 2: Customized Unsteady Inlet Boundary Condition in the FINE/Open-manual is the following equation.
This is the same question as the one in the OpenLabs section "Unsteady inlet boundary condition with OpenLabs"?If not, could you please elaborate on the difference?Best regards,Colinda
Hey, oh yes sry. Problem is solved, i use the functions of the fourier series, greetings Hussein