<?xml version="1.0" encoding="UTF-8"?>
<AeolusASP>
    <Info version="4.20" timestamp="20/10/2021 10:11:20"/>
    <Model type="aircraft">
        <UnitSystem type="si10"/>
        <Wings>
            <Wing name="Main wing" color="0.0 0.5450000166893005 0.8199999928474426">
                <Geometry origin="0.0 0.0 0.0" epsilon_ref="0.0" scale="1.0">
                    <Settings chordMode="0"/>
                    <Airfoils>
                        <Airfoil name="MS33_13GP" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.0" l="1.0" alpha_wt="0.0" phi="30.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="MS33_13GP" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.25" l="1.0" alpha_wt="0.0" phi="30.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="MS33_13GP" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="2.5" l="1.0" alpha_wt="0.0" phi="30.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="MS33_13GP" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="3.75" l="1.0" alpha_wt="0.0" phi="30.0" dihedral="10.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="MS33_13GP" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="5.0" l="1.0" alpha_wt="0.0" phi="10.0" dihedral="80.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA0012" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="6.0" l="1.0" alpha_wt="0.0" phi="10.0" dihedral="100.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="MS33_13GP" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="7.0" l="1.0" alpha_wt="0.0" phi="20.0" dihedral="170.0" inverted="true" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="MS33_13GP" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="8.15" l="1.0" alpha_wt="0.0" phi="20.0" dihedral="180.0" inverted="true" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="MS33_13GP" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="9.3" l="1.0" alpha_wt="0.0" phi="20.0" dihedral="180.0" inverted="true" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="MS33_13GP" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="10.45" l="1.0" alpha_wt="0.0" phi="20.0" dihedral="180.0" inverted="true" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="MS33_13GP" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="11.6079" l="1.0" alpha_wt="0.0" phi="0.0" dihedral="180.0" inverted="true" flapchord="0.2" flapdeflection="0.0"/>
                    </Airfoils>
                </Geometry>
                <Discretization smooth="true" npwingstrip="42">
                    <Strip stripdensity="0.3" type="Constant"/>
                    <Strip stripdensity="0.3" type="Constant"/>
                    <Strip stripdensity="0.3" type="Constant"/>
                    <Strip stripdensity="0.3" type="Constant"/>
                    <Strip stripdensity="0.3" type="Constant"/>
                    <Strip stripdensity="0.3" type="Constant"/>
                    <Strip stripdensity="0.3" type="Constant"/>
                    <Strip stripdensity="0.3" type="Constant"/>
                    <Strip stripdensity="0.3" type="Constant"/>
                    <Strip stripdensity="0.3" type="Constant"/>
                </Discretization>
            </Wing>
        </Wings>
        <Propulsion>
        </Propulsion>
        <FlightCondition aircraftWeight="6615.0" fluid="air" altitude="2000.0" temperature="15.0" trueSpeed="30.0" cdviscwet="0.005"/>
        <Computation symmetry="true" numberOfCores="8" aoa="-3.0 5.0 10.0 " nsubpanels="15" normalizedzetaoffset="0.005" wakelengthfactor="1000.0" normalizedfarfield="5.0"/>
        <Optimization enabled="true">
            <GoalType goalType="maximize"/>
            <ObjectiveFunction objective="currentE"/>
            <DesignVariables>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 10 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 7 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 9 "/>
                <DesignVariable min="0.5" max="1.5" key="wing 0 chord 4 "/>
                <DesignVariable min="0.5" max="1.5" key="wing 0 chord 3 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 3 "/>
                <DesignVariable min="0.5" max="1.5" key="wing 0 chord 8 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 0 "/>
                <DesignVariable min="0.5" max="1.5" key="wing 0 chord 5 "/>
                <DesignVariable min="0.5" max="1.5" key="wing 0 chord 9 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 8 "/>
                <DesignVariable min="0.5" max="1.5" key="wing 0 chord 10 "/>
                <DesignVariable min="0.5" max="1.5" key="wing 0 chord 0 "/>
                <DesignVariable min="0.5" max="1.5" key="wing 0 chord 6 "/>
                <DesignVariable min="0.5" max="1.5" key="wing 0 chord 1 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 4 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 6 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 1 "/>
                <DesignVariable min="0.5" max="1.5" key="wing 0 chord 2 "/>
                <DesignVariable min="0.5" max="1.5" key="wing 0 chord 7 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 5 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 2 "/>
            </DesignVariables>
            <Constraints>
                <Constraint type="Local Cl_wet" target="" min="" max="0.5" weight="100.0"/>
                <Constraint type="Static margin" target="" min="0.025" max="" weight="100.0"/>
            </Constraints>
            <Optimizer algorithm="CMA-ES" maxEvaluations="100000"/>
        </Optimization>
        <ParamaterStudies enabled="true" nsteps="20">
            <ObjectiveFunction objective="requiredperformance"/>
            <DesignVariables>
                <DesignVariable min="10.0" max="50.0" key="flightcondition truespeed "/>
            </DesignVariables>
        </ParamaterStudies>
    </Model>
</AeolusASP>