<?xml version="1.0" encoding="UTF-8"?>
<AeolusASP>
    <Info version="4.23" timestamp="10/08/2022 12:49:21"/>
    <Model type="aircraft" name="UAV">
        <UnitSystem type="si10"/>
        <Wings>
            <Wing name="Wing" color="0.0 0.5450000166893005 0.8199999928474426">
                <Geometry origin="0.0 0.0 0.0" epsilon_ref="0.8031806322987101" scale="1.0">
                    <Settings chordMode="0"/>
                    <Airfoils>
                        <Airfoil name="NACA632615" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.0" l="0.42" alpha_wt="0.0" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA632615" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.53" l="0.42" alpha_wt="-0.36" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA632615" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.54" l="0.31" alpha_wt="-1.38" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA632615" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.8" l="0.236" alpha_wt="-0.41" phi="-1.41" dihedral="8.5" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA632615" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.9" l="0.205" alpha_wt="-1.7" phi="-4.0" dihedral="9.5" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA632615" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.95" l="0.174" alpha_wt="-2.1" phi="-1.96" dihedral="45.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA632615" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="2.0" l="0.145" alpha_wt="-0.29" phi="-5.01" dihedral="75.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA632615" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="2.05" l="0.14" alpha_wt="-1.3" phi="-1.66" dihedral="90.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA632615" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="2.15" l="0.103" alpha_wt="1.9" phi="7.89" dihedral="90.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="RAF30" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="2.3" l="0.04" alpha_wt="-2.3" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                    </Airfoils>
                </Geometry>
                <Discretization smooth="false" npwingstrip="48">
                    <Strip stripdensity="0.2" type="Outboard"/>
                    <Strip stripdensity="0.2" type="Both"/>
                    <Strip stripdensity="0.3" type="Outboard"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.8" type="Constant"/>
                    <Strip stripdensity="0.8" type="Constant"/>
                    <Strip stripdensity="0.8" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                </Discretization>
            </Wing>
            <Wing name="Tailplane" color="1.0 0.800000011920929 0.0">
                <Geometry origin="1.5 0.0 0.45" epsilon_ref="0.75" scale="1.0">
                    <Settings chordMode="0"/>
                    <Airfoils>
                        <Airfoil name="NACA0012" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.0" l="0.3" alpha_wt="0.0" phi="0.0" dihedral="-35.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA0012" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.7" l="0.3" alpha_wt="0.0" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                    </Airfoils>
                </Geometry>
                <Discretization smooth="false" npwingstrip="48">
                    <Strip stripdensity="0.2" type="Both"/>
                </Discretization>
            </Wing>
        </Wings>
        <Propulsion>
            <Propeller name="Prop 1" base="0.35 0.0 -0.15" angle="0.0" diameter="0.7" thrust="0.0" color="0.501960813999176 0.501960813999176 0.501960813999176" pusher="true"/>
        </Propulsion>
        <FlightCondition aircraftWeight="392.0" fluid="air" altitude="500.0" temperature="22.0" trueSpeed="25.0" cdviscwet="0.005"/>
        <Computation symmetry="true" numberOfCores="4" 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="0.1" max="0.3" key="wing 0 chord 5 "/>
                <DesignVariable min="0.1" max="0.3" key="wing 0 chord 6 "/>
                <DesignVariable min="-30.0" max="30.0" key="wing 0 sweep 3 "/>
                <DesignVariable min="0.1" max="0.3" key="wing 0 chord 3 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 6 "/>
                <DesignVariable min="0.05" max="0.3" key="wing 0 chord 8 "/>
                <DesignVariable min="0.04" max="0.3" key="wing 0 chord 9 "/>
                <DesignVariable min="2.22" max="2.3" key="wing 0 s 9 "/>
                <DesignVariable min="-5.0" max="5.0" key="wing 0 twist 1 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 7 "/>
                <DesignVariable min="-30.0" max="30.0" key="wing 0 sweep 8 "/>
                <DesignVariable min="-30.0" max="30.0" key="wing 0 sweep 6 "/>
                <DesignVariable min="0.1" max="0.3" key="wing 0 chord 4 "/>
                <DesignVariable min="-30.0" max="30.0" key="wing 0 sweep 4 "/>
                <DesignVariable min="-5.0" max="5.0" key="wing 0 twist 3 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 8 "/>
                <DesignVariable min="-20.0" max="20.0" key="wing 0 dihedral 3 "/>
                <DesignVariable min="-0.25" max="1.25" key="wing 0 epsref "/>
                <DesignVariable min="-5.0" max="5.0" key="wing 0 twist 2 "/>
                <DesignVariable min="-30.0" max="30.0" key="wing 0 sweep 5 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 9 "/>
                <DesignVariable min="-30.0" max="30.0" key="wing 0 sweep 7 "/>
                <DesignVariable min="0.05" max="0.3" key="wing 0 chord 7 "/>
                <DesignVariable min="-20.0" max="20.0" key="wing 0 dihedral 4 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 5 "/>
                <DesignVariable min="-10.0" max="10.0" key="wing 0 twist 4 "/>
            </DesignVariables>
            <Constraints>
                <Constraint type="Local Cl_wet" target="Wing" min="" max="0.38" weight="50.0"/>
            </Constraints>
            <Optimizer algorithm="CMA-ES" maxEvaluations="10000000"/>
        </Optimization>
        <ParamaterStudies enabled="false" nsteps="20">
            <ObjectiveFunction objective="currentE"/>
        </ParamaterStudies>
    </Model>
</AeolusASP>