<?xml version="1.0" encoding="UTF-8"?>
<AeolusASP>
    <Info version="4.25" timestamp="03/09/2022 16:47:22"/>
    <Model type="propeller" nblades="2" rpm="-1550.0" adjustment="-4.875" name="Default_Propeller">
        <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="PROP_NACA339_9FT_0185" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.254" l="0.1593" alpha_wt="-50.3" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="PROP_NACA339_9FT_0222" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.3048" l="0.1661" alpha_wt="-52.4" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="PROP_NACA339_9FT_0333" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.4572" l="0.1808" alpha_wt="-57.7" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="PROP_NACA339_9FT_0444" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.6096" l="0.1842" alpha_wt="-62.2" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="PROP_NACA339_9FT_0556" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.762" l="0.1796" alpha_wt="-65.6" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="PROP_NACA339_9FT_0667" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.9144" l="0.1638" alpha_wt="-68.2" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="PROP_NACA339_9FT_0778" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.0668" l="0.1377" alpha_wt="-70.1" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="PROP_NACA339_9FT_0889" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.2192" l="0.1029" alpha_wt="-71.7" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="PROP_NACA339_9FT_0944" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.2954" l="0.0841" alpha_wt="-72.4" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="PROP_NACA339_9FT_0944" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.352" l="0.071" alpha_wt="-72.9" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                    </Airfoils>
                </Geometry>
                <Discretization smooth="true" npwingstrip="52">
                    <Strip stripdensity="0.4" type="Constant"/>
                    <Strip stripdensity="0.4" type="Constant"/>
                    <Strip stripdensity="0.4" type="Constant"/>
                    <Strip stripdensity="0.4" type="Constant"/>
                    <Strip stripdensity="0.4" type="Constant"/>
                    <Strip stripdensity="0.4" type="Constant"/>
                    <Strip stripdensity="0.4" type="Constant"/>
                    <Strip stripdensity="0.4" type="Constant"/>
                    <Strip stripdensity="0.4" type="Constant"/>
                </Discretization>
            </Wing>
        </Wings>
        <FlightCondition aircraftWeight="0.0" fluid="air" altitude="370.0" temperature="0.0" trueSpeed="30.0" 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="maximize"/>
            <ObjectiveFunction objective="propeller_thrust"/>
            <Optimizer algorithm="BOBYQA" maxEvaluations="1000"/>
        </Optimization>
        <ParamaterStudies enabled="true" nsteps="10">
            <ObjectiveFunction objective="propeller_thrust"/>
            <DesignVariables>
                <DesignVariable min="20.0" max="54.0" key="flightcondition truespeed "/>
            </DesignVariables>
        </ParamaterStudies>
    </Model>
</AeolusASP>