<?xml version="1.0" encoding="utf-8"?><Code_Saturne_GUI case="Rotor_37" solver_version="4.0" study="Code_Saturne_Simulation" version="2.0">
	<additional_scalars/>
	<analysis_control>
		<output>
			<listing_printing_frequency>1</listing_printing_frequency>
			<mesh id="-1" label="Fluid domain" type="cells">
				<all_variables status="on"/>
				<location>all[]</location>
				<writer id="-1"/>
			</mesh>
			<mesh id="-2" label="Boundary" type="boundary_faces">
				<all_variables status="on"/>
				<location>all[]</location>
				<writer id="-1"/>
			</mesh>
			<probe_format choice="DAT"/>
			<probe_recording_frequency>1</probe_recording_frequency>
			<writer id="-1" label="results">
				<directory name="postprocessing"/>
				<format name="ensight" options="binary"/>
				<frequency period="none"/>
				<output_at_end status="on"/>
				<time_dependency choice="fixed_mesh"/>
			</writer>
		</output>
		<profiles/>
		<steady_management status="off"/>
		<time_averages/>
		<time_parameters>
			<iterations>10000</iterations>
			<max_courant_num>0.8</max_courant_num>
			<max_fourier_num>10</max_fourier_num>
			<property label="CourantNb" name="courant_number"/>
			<property label="FourierNb" name="fourier_number">
				<listing_printing status="off"/>
			</property>
			<property label="LocalTime" name="local_time_step">
				<postprocessing_recording status="off"/>
			</property>
			<time_passing>1</time_passing>
			<time_step_max_factor>1000</time_step_max_factor>
			<time_step_min_factor>0.1</time_step_min_factor>
			<time_step_ref>1e-09</time_step_ref>
			<time_step_var>0.1</time_step_var>
			<zero_time_step status="off"/>
		</time_parameters>
	</analysis_control>
	<boundary_conditions>
		<boundary label="BC_1" name="1" nature="wall">BLADE_HUB_ROTATING</boundary>
		<boundary label="BC_2" name="2" nature="wall">HUB_STATIONARY</boundary>
		<boundary label="BC_3" name="3" nature="inlet">INLET</boundary>
		<boundary label="BC_4" name="4" nature="outlet">OUTLET</boundary>
		<boundary label="BC_5" name="5" nature="wall">SHROUD</boundary>
		<boundary label="BC_6" name="6" nature="symmetry">SYMMETRY</boundary>
		<inlet label="BC_3">
			<turbulence choice="turbulent_intensity">
				<hydraulic_diameter>0.16</hydraulic_diameter>
				<turbulent_intensity>3</turbulent_intensity>
			</turbulence>
			<velocity_pressure choice="norm" direction="normal">
				<compressible_type choice="subsonic_inlet_PH"/>
				<enthalpy status="on">289850</enthalpy>
				<norm>1</norm>
				<total_pressure status="on">101325</total_pressure>
			</velocity_pressure>
		</inlet>
		<outlet label="BC_4">
			<compressible_type choice="subsonic_outlet"/>
			<dirichlet name="pressure">90000</dirichlet>
		</outlet>
		<symmetry label="BC_6"/>
		<variable/>
		<wall label="BC_1">
			<velocity_pressure choice="off">
				<dirichlet component="0" name="velocity">0</dirichlet>
				<dirichlet component="1" name="velocity">0</dirichlet>
				<dirichlet component="2" name="velocity">0</dirichlet>
			</velocity_pressure>
		</wall>
		<wall label="BC_2">
			<velocity_pressure choice="off"/>
		</wall>
		<wall label="BC_5">
			<velocity_pressure choice="off"/>
		</wall>
	</boundary_conditions>
	<calculation_management>
		<block_io/>
		<partitioning/>
		<start_restart>
			<frozen_field status="off"/>
		</start_restart>
	</calculation_management>
	<lagrangian model="off">
		<output/>
	</lagrangian>
	<numerical_parameters>
		<gradient_reconstruction choice="0"/>
		<gradient_transposed status="on"/>
		<hydrostatic_equilibrium status="on"/>
		<hydrostatic_pressure status="off"/>
		<pressure_relaxation>1</pressure_relaxation>
		<velocity_pressure_algo choice="simplec">
			<piso_sweep_number>1</piso_sweep_number>
		</velocity_pressure_algo>
		<velocity_pressure_coupling status="off"/>
		<wall_pressure_extrapolation>0</wall_pressure_extrapolation>
	</numerical_parameters>
	<physical_properties>
		<fluid_properties>
			<material choice="user_material"/>
			<method choice="user_properties"/>
			<property choice="variable" label="Density" name="density">
				<formula status="off" zone_id="1"/>
				<initial_value>1.2758</initial_value>
			</property>
			<property choice="constant" label="DiffDyn" name="dynamic_diffusion">
				<initial_value>0.01</initial_value>
				<listing_printing status="off"/>
				<postprocessing_recording status="off"/>
			</property>
			<property choice="constant" label="LamVisc" name="molecular_viscosity">
				<initial_value>1.7218e-05</initial_value>
				<listing_printing status="off"/>
				<postprocessing_recording status="off"/>
			</property>
			<property choice="constant" label="SpecHeat" name="specific_heat">
				<initial_value>1005.9</initial_value>
				<listing_printing status="off"/>
				<postprocessing_recording status="off"/>
			</property>
			<property choice="constant" label="ThermalCond" name="thermal_conductivity">
				<initial_value>0.02436</initial_value>
				<listing_printing status="off"/>
				<postprocessing_recording status="off"/>
			</property>
			<property choice="constant" label="VolVisc" name="volume_viscosity">
				<initial_value>0</initial_value>
				<listing_printing status="off"/>
				<postprocessing_recording status="off"/>
			</property>
			<reference choice="user_material"/>
		</fluid_properties>
		<gravity>
			<gravity_x>0</gravity_x>
			<gravity_y>0</gravity_y>
			<gravity_z>0</gravity_z>
		</gravity>
		<omega>
			<omega_x>0</omega_x>
			<omega_y>0</omega_y>
			<omega_z>0</omega_z>
		</omega>
	</physical_properties>
	<solution_domain>
		<faces_cutting status="off"/>
		<joining/>
		<mesh_smoothing status="off"/>
		<meshes_list>
			<mesh name="Rotor37.cgns" path="R:/W0158_Chris Kemmerzell/IPA/ACAT_Rotor_1/NASA_Rotor37/Code_Saturne_Simulation/MESH"/>
		</meshes_list>
		<periodicity/>
		<volumic_conditions>
			<zone darcy_law="off" head_losses="off" id="1" initialization="on" label="all_cells" mass_source_term="off" momentum_source_term="off" porosity="off" scalar_source_term="off" thermal_source_term="off">all[]</zone>
		</volumic_conditions>
	</solution_domain>
	<thermophysical_models>
		<ale_method status="off"/>
		<atmospheric_flows model="off"/>
		<compressible_model model="constant_gamma">
			<variable label="temperature" name="temperature" type="model">
				<formula status="on" zone_id="1">temperature = 273.15;</formula>
				<rhs_reconstruction>1</rhs_reconstruction>
			</variable>
		</compressible_model>
		<conjugate_heat_transfer>
			<external_coupling/>
		</conjugate_heat_transfer>
		<darcy_model model="off"/>
		<gas_combustion model="off" option="off"/>
		<joule_effect model="off"/>
		<radiative_transfer model="off"/>
		<reference_values>
			<mass_molar>0.028966</mass_molar>
			<pressure>101325</pressure>
			<temperature>273.15</temperature>
			<velocity>1</velocity>
		</reference_values>
		<solid_fuels model="off"/>
		<thermal_scalar model="total_energy">
			<property label="Dimensionless Thermal flux" name="boundary_layer_nusselt" support="boundary">
				<postprocessing_recording status="off"/>
			</property>
			<property label="Boundary temperature" name="boundary_temperature" support="boundary"/>
			<property label="Thermal flux" name="thermal_flux" support="boundary"/>
			<property label="Tplus" name="tplus" support="boundary">
				<postprocessing_recording status="off"/>
			</property>
			<variable label="TotEner" name="total_energy" type="thermal">
				<formula status="off" zone_id="1"/>
				<listing_printing status="off"/>
				<max_value>1e+12</max_value>
				<min_value>0</min_value>
				<rhs_reconstruction>1</rhs_reconstruction>
				<turbulent_flux_model>SGDH</turbulent_flux_model>
			</variable>
		</thermal_scalar>
		<turbomachinery model="frozen">
			<joining/>
			<rotor rotor_id="0">
				<criteria>BLADE_HUB_ROTATING</criteria>
				<rotation>
					<axis_x>0</axis_x>
					<axis_y>0</axis_y>
					<axis_z>-1</axis_z>
					<invariant_x>0</invariant_x>
					<invariant_y>0</invariant_y>
					<invariant_z>0</invariant_z>
				</rotation>
				<velocity status="constant">
					<value>1800</value>
				</velocity>
			</rotor>
		</turbomachinery>
		<turbulence model="k-omega-SST">
			<gravity_terms status="on"/>
			<initialization choice="reference_value" zone_id="1"/>
			<property label="TurbVisc" name="turbulent_viscosity">
				<listing_printing status="off"/>
			</property>
			<scale_model>1</scale_model>
			<variable label="k" name="k">
				<listing_printing status="off"/>
				<rhs_reconstruction>1</rhs_reconstruction>
			</variable>
			<variable label="omega" name="omega">
				<listing_printing status="off"/>
				<rhs_reconstruction>1</rhs_reconstruction>
			</variable>
		</turbulence>
		<velocity_pressure>
			<initialization>
				<formula zone_id="1">velocity[0] = 0.;
velocity[1] = 0.;
velocity[2] = 0.;</formula>
			</initialization>
			<property label="Efforts" name="effort" support="boundary"/>
			<property label="Efforts, normal" name="effort_normal" support="boundary">
				<postprocessing_recording status="off"/>
			</property>
			<property label="Efforts, tangential" name="effort_tangential" support="boundary">
				<postprocessing_recording status="off"/>
			</property>
			<property label="total_pressure" name="total_pressure"/>
			<property label="Yplus" name="yplus" support="boundary"/>
			<variable label="Pressure" name="pressure">
				<formula status="on" zone_id="1">p0 = 101325;
pressure = p0;</formula>
				<rhs_reconstruction>2</rhs_reconstruction>
			</variable>
			<variable dimension="3" label="Velocity" name="velocity">
				<rhs_reconstruction>1</rhs_reconstruction>
			</variable>
		</velocity_pressure>
	</thermophysical_models>
</Code_Saturne_GUI>