<?xml version="1.0" encoding="UTF-8"?>
<AeolusASP>
    <Info version="4.25" timestamp="03/09/2022 16:41:05"/>
    <Model type="propeller" nblades="2" rpm="-1500.0" adjustment="-80.0" name="Boxprop">
        <UnitSystem type="si10"/>
        <Wings>
            <Wing name="Blade" color="0.0 0.5450000166893005 0.8199999928474426">
                <Geometry origin="0.0 0.0 0.0" epsilon_ref="0.446" scale="1.0">
                    <Settings chordMode="0"/>
                    <Airfoils>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.075" l="0.05" alpha_wt="30.0" phi="0.0" dihedral="-5.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.14375" l="0.05" alpha_wt="20.0" phi="0.0" dihedral="-5.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.21249999999999997" l="0.05" alpha_wt="15.0" phi="0.0" dihedral="-5.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.28125" l="0.0475" alpha_wt="10.0" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.35" l="0.04" alpha_wt="10.0" phi="0.0" dihedral="15.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.3758819045102521" l="0.035" alpha_wt="5.0" phi="0.0" dihedral="45.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.4017638090205041" l="0.035" alpha_wt="0.0" phi="0.0" dihedral="75.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA0015" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.4276457135307562" l="0.035" alpha_wt="0.0" phi="0.0" dihedral="105.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.4535276180410083" l="0.035" alpha_wt="0.0" phi="0.0" dihedral="135.0" inverted="true" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.47940952255126035" l="0.035" alpha_wt="-5.0" phi="0.0" dihedral="165.0" inverted="true" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.5052914270615124" l="0.04" alpha_wt="-10.0" phi="0.0" dihedral="180.0" inverted="true" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.5740414270615124" l="0.0475" alpha_wt="-10.0" phi="0.0" dihedral="185.0" inverted="true" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.6427914270615125" l="0.05" alpha_wt="-15.0" phi="0.0" dihedral="185.0" inverted="true" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.7115414270615126" l="0.05" alpha_wt="-20.0" phi="0.0" dihedral="185.0" inverted="true" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA4412" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.7802914270615126" l="0.05" alpha_wt="-30.0" phi="0.0" dihedral="95.0" inverted="true" flapchord="0.2" flapdeflection="0.0"/>
                    </Airfoils>
                </Geometry>
                <Discretization smooth="true" npwingstrip="48">
                    <Strip stripdensity="0.2" type="Constant"/>
                    <Strip stripdensity="0.2" type="Constant"/>
                    <Strip stripdensity="0.2" type="Constant"/>
                    <Strip stripdensity="0.2" type="Constant"/>
                    <Strip stripdensity="0.2" type="Constant"/>
                    <Strip stripdensity="0.2" type="Constant"/>
                    <Strip stripdensity="0.2" type="Constant"/>
                    <Strip stripdensity="0.2" type="Constant"/>
                    <Strip stripdensity="0.2" type="Constant"/>
                    <Strip stripdensity="0.2" type="Constant"/>
                    <Strip stripdensity="0.2" type="Constant"/>
                    <Strip stripdensity="0.2" type="Constant"/>
                    <Strip stripdensity="0.2" type="Constant"/>
                    <Strip stripdensity="0.2" type="Constant"/>
                </Discretization>
            </Wing>
        </Wings>
        <FlightCondition aircraftWeight="0.0" fluid="air" altitude="370.0" temperature="0.0" trueSpeed="10.0" cdviscwet="0.005"/>
        <Computation symmetry="false" numberOfCores="16" aoa="-3.0 5.0 10.0 " nsubpanels="15" normalizedzetaoffset="0.005" wakelengthfactor="5.0" normalizedfarfield="5.0"/>
        <Optimization enabled="false">
            <GoalType goalType="minimize"/>
            <ObjectiveFunction objective="propeller_shaftpower"/>
            <Optimizer algorithm="CMA-ES" maxEvaluations="50000"/>
        </Optimization>
        <ParamaterStudies enabled="true" nsteps="20">
            <ObjectiveFunction objective="propeller_efficiency"/>
            <DesignVariables>
                <DesignVariable min="10.0" max="19.0" key="flightcondition truespeed "/>
            </DesignVariables>
        </ParamaterStudies>
    </Model>
</AeolusASP>