<?xml version="1.0" encoding="utf-8"?><Code_Saturne_GUI case="K-OMEGA_SST" study="2d_flaps_v2.3" version="2.0">
	<solution_domain>
		<volumic_conditions>
			<zone head_losses="off" id="1" initialization="on" label="all_cells" mass_source_term="off" momentum_source_term="off" scalar_source_term="off" thermal_source_term="off">all[]</zone>
		</volumic_conditions>
		<meshes_list>
			<mesh name="flaps.med"/>
		</meshes_list>
		<faces_cutting status="off"/>
		<mesh_smoothing status="off"/>
		<joining/>
		<periodicity/>
	</solution_domain>
	<thermophysical_models>
		<velocity_pressure>
			<variable label="Pressure" name="pressure">
				<solver_precision>1e-05</solver_precision>
			</variable>
			<variable label="VelocityX" name="velocity_U">
				<rhs_reconstruction>1</rhs_reconstruction>
				<solver_precision>1e-05</solver_precision>
				<blending_factor>1</blending_factor>
			</variable>
			<variable label="VelocityY" name="velocity_V">
				<rhs_reconstruction>1</rhs_reconstruction>
				<solver_precision>1e-05</solver_precision>
				<blending_factor>1</blending_factor>
			</variable>
			<variable label="VelocityZ" name="velocity_W">
				<rhs_reconstruction>1</rhs_reconstruction>
				<solver_precision>1e-05</solver_precision>
				<blending_factor>1</blending_factor>
			</variable>
			<property label="total_pressure" name="total_pressure"/>
			<property label="Yplus" name="yplus" support="boundary"/>
			<property label="Efforts" name="effort" support="boundary"/>
			<property label="all_variables" name="all_variables" support="boundary"/>
			<initialization>
				<formula zone_id="1">u = 0;
v = 0;
w = 0;</formula>
			</initialization>
		</velocity_pressure>
		<reference_values>
			<pressure>101325</pressure>
			<velocity>1</velocity>
			<temperature>1273.15</temperature>
		</reference_values>
		<turbulence model="k-omega-SST">
			<variable label="TurbEner" name="turb_k">
				<rhs_reconstruction>1</rhs_reconstruction>
				<solver_precision>1e-05</solver_precision>
			</variable>
			<property label="TurbVisc" name="turb_viscosity"/>
			<initialization choice="reference_value" zone_id="1"/>
			<variable label="omega" name="turb_omega">
				<rhs_reconstruction>1</rhs_reconstruction>
				<solver_precision>1e-05</solver_precision>
			</variable>
			<scale_model>1</scale_model>
			<gravity_terms status="on"/>
		</turbulence>
		<ale_method status="off"/>
		<thermal_scalar model="temperature_celsius">
			<property label="input_thermal_flux" name="input_thermal_flux" support="boundary"/>
		</thermal_scalar>
		<radiative_transfer model="off">
			<restart status="off"/>
			<absorption_coefficient type="constant">0</absorption_coefficient>
		</radiative_transfer>
		<conjugate_heat_transfer>
			<external_coupling/>
		</conjugate_heat_transfer>
		<compressible_model model="off"/>
		<solid_fuels model="off"/>
		<gas_combustion model="off" option="2-peak_adiabatic"/>
		<joule_effect model="off"/>
		<atmospheric_flows model="off"/>
		<heads_losses/>
	</thermophysical_models>
	<numerical_parameters>
		<velocity_pressure_algo choice="simplec">
			<piso_sweep_number>1</piso_sweep_number>
		</velocity_pressure_algo>
		<gradient_transposed status="on"/>
		<velocity_pressure_coupling status="off"/>
		<hydrostatic_pressure status="off"/>
		<pressure_relaxation>1</pressure_relaxation>
		<wall_pressure_extrapolation>0</wall_pressure_extrapolation>
		<gradient_reconstruction choice="0"/>
	</numerical_parameters>
	<physical_properties>
		<fluid_properties>
			<property choice="constant" label="Density" name="density">
				<listing_printing status="off"/>
				<postprocessing_recording status="off"/>
				<initial_value>1.17862</initial_value>
			</property>
			<property choice="constant" label="LamVisc" name="molecular_viscosity">
				<listing_printing status="off"/>
				<postprocessing_recording status="off"/>
				<initial_value>1.83e-05</initial_value>
			</property>
			<property choice="constant" label="SpecHeat" name="specific_heat">
				<listing_printing status="off"/>
				<postprocessing_recording status="off"/>
				<initial_value>1017.24</initial_value>
			</property>
			<property choice="constant" label="ThermalCond" name="thermal_conductivity">
				<listing_printing status="off"/>
				<postprocessing_recording status="off"/>
				<initial_value>0.02495</initial_value>
			</property>
			<property choice="constant" label="DiffDyn" name="dynamic_diffusion">
				<listing_printing status="off"/>
				<postprocessing_recording status="off"/>
				<initial_value>0.01</initial_value>
			</property>
		</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>
	<additional_scalars>
		<scalar label="TempC" name="temperature_celsius" type="thermal">
			<rhs_reconstruction>1</rhs_reconstruction>
			<min_value>-273.15</min_value>
			<max_value>1e+12</max_value>
			<solver_precision>1e-05</solver_precision>
			<formula zone_id="1">TempC = 20;</formula>
			<blending_factor>1</blending_factor>
		</scalar>
	</additional_scalars>
	<boundary_conditions>
		<boundary label="farfield" name="1" nature="inlet">farfield</boundary>
		<inlet label="farfield">
			<velocity_pressure choice="norm" direction="coordinates">
				<norm>53</norm>
				<direction_x>1</direction_x>
				<direction_y>0</direction_y>
				<direction_z>0</direction_z>
			</velocity_pressure>
			<turbulence choice="hydraulic_diameter">
				<hydraulic_diameter>1</hydraulic_diameter>
			</turbulence>
			<scalar choice="dirichlet" label="TempC" name="temperature_celsius" type="thermal">
				<dirichlet>20</dirichlet>
			</scalar>
		</inlet>
		<boundary label="symm2" name="3" nature="symmetry">symm2</boundary>
		<boundary label="symm1" name="4" nature="symmetry">symm1</boundary>
		<symmetry label="symm1"/>
		<boundary label="slat" name="5" nature="wall">slat</boundary>
		<symmetry label="symm2"/>
		<wall label="slat">
			<velocity_pressure choice="off">
				<dirichlet name="velocity_U">0</dirichlet>
				<dirichlet name="velocity_V">0</dirichlet>
				<dirichlet name="velocity_W">0</dirichlet>
			</velocity_pressure>
			<scalar choice="neumann" label="TempC" name="temperature_celsius" type="thermal">
				<neumann>0</neumann>
			</scalar>
		</wall>
		<boundary label="flap" name="6" nature="wall">flap</boundary>
		<wall label="flap">
			<velocity_pressure choice="off"/>
			<scalar choice="neumann" label="TempC" name="temperature_celsius" type="thermal">
				<neumann>0</neumann>
			</scalar>
		</wall>
		<boundary label="wing" name="7" nature="wall">wing</boundary>
		<wall label="wing">
			<velocity_pressure choice="off"/>
			<scalar choice="neumann" label="TempC" name="temperature_celsius" type="thermal">
				<neumann>0</neumann>
			</scalar>
		</wall>
		<boundary label="out" name="8" nature="inlet">out</boundary>
		<inlet label="out">
			<velocity_pressure choice="norm" direction="coordinates">
				<norm>53</norm>
				<direction_x>1</direction_x>
				<direction_y>0</direction_y>
				<direction_z>0</direction_z>
			</velocity_pressure>
			<turbulence choice="hydraulic_diameter">
				<hydraulic_diameter>1</hydraulic_diameter>
			</turbulence>
			<scalar choice="dirichlet" label="TempC" name="temperature_celsius" type="thermal">
				<dirichlet>20</dirichlet>
			</scalar>
		</inlet>
		<variable/>
	</boundary_conditions>
	<analysis_control>
		<output>
			<writer id="-1" label="results">
				<frequency period="none"/>
				<output_at_end status="on"/>
				<format name="ensight" options="binary"/>
				<directory name="postprocessing"/>
				<time_dependency choice="fixed_mesh"/>
			</writer>
			<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>
			<listing_printing_frequency>1</listing_printing_frequency>
			<probe_recording_frequency>1</probe_recording_frequency>
			<probe_format choice="DAT"/>
			<probe name="1" status="on">
				<probe_x>-0.37</probe_x>
				<probe_y>-0.5</probe_y>
				<probe_z>3.9</probe_z>
			</probe>
			<probe name="2" status="on">
				<probe_x>3.6</probe_x>
				<probe_y>-0.5</probe_y>
				<probe_z>-2.8</probe_z>
			</probe>
			<probe name="3" status="on">
				<probe_x>8.9</probe_x>
				<probe_y>-0.5</probe_y>
				<probe_z>0.35</probe_z>
			</probe>
			<probe name="4" status="on">
				<probe_x>0.012</probe_x>
				<probe_y>-0.5</probe_y>
				<probe_z>-0.03156</probe_z>
			</probe>
			<probe name="5" status="on">
				<probe_x>-0.7328</probe_x>
				<probe_y>-0.5</probe_y>
				<probe_z>-0.0727</probe_z>
			</probe>
			<probe name="6" status="on">
				<probe_x>0.46313</probe_x>
				<probe_y>-0.5</probe_y>
				<probe_z>0.10545</probe_z>
			</probe>
			<probe name="7" status="on">
				<probe_x>0.4631</probe_x>
				<probe_y>-0.5</probe_y>
				<probe_z>-0.06695</probe_z>
			</probe>
			<probe name="8" status="on">
				<probe_x>0.7251</probe_x>
				<probe_y>-0.5</probe_y>
				<probe_z>-0.007423</probe_z>
			</probe>
			<probe name="9" status="on">
				<probe_x>0.90387</probe_x>
				<probe_y>-0.5</probe_y>
				<probe_z>0.04025</probe_z>
			</probe>
			<probe name="10" status="on">
				<probe_x>0.89</probe_x>
				<probe_y>-0.5</probe_y>
				<probe_z>-0.0165315</probe_z>
			</probe>
			<probe name="11" status="on">
				<probe_x>1.218</probe_x>
				<probe_y>-0.5</probe_y>
				<probe_z>-0.13025</probe_z>
			</probe>
		</output>
		<time_parameters>
			<time_step_ref>0.0002</time_step_ref>
			<iterations>5000</iterations>
			<time_passing>0</time_passing>
			<property label="CourantNb" name="courant_number"/>
			<property label="FourierNb" name="fourier_number"/>
			<zero_time_step status="off"/>
		</time_parameters>
		<steady_management status="off"/>
		<time_averages/>
		<profiles/>
	</analysis_control>
	<calculation_management>
		<start_restart>
			<frozen_field status="off"/>
			<restart_rescue>0</restart_rescue>
			<restart_with_auxiliary status="on"/>
		</start_restart>
		<partitioning>
			<rank_step>4</rank_step>
		</partitioning>
		<n_procs>4</n_procs>
		<run_type>standard</run_type>
	</calculation_management>
	<lagrangian model="off"/>
</Code_Saturne_GUI>