Characterization of Flow Interactions in a One-Stage Shrouded Axial Turbine

Table 2

Boundary conditions.

Fluid	Combustion gas mixture
Inlet conditions	Total pressure 1.539 MPa & total temperature = 1335.15 K; Turbulence intensity~5% & length scale = 0.1 ×
Outlet conditions	Static pressure: Pa
Wall conditions	NGV		Rotor
	Vane	No slip stationary wall	Blade	No slip rotating wall
	Hub	No slip stationary wall	Hub	No slip stationary wall
	Shroud	No slip stationary wall	Shroud	Counterrotating wall
Lateral surfaces	Periodicity
Interface in steady simulations	Frozen and stage interface
Interface in unsteady simulations	Transient rotor/stator interface