<?xml version="1.0" encoding="UTF-8"?>
<AeolusASP>
    <Info version="4.14" timestamp="06/09/2020 20:19:09"/>
    <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">
                    <Settings chordMode="0"/>
                    <Airfoils>
                        <Airfoil name="NACA644221" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.0" l="2.5" alpha_wt="7.0" phi="33.0" dihedral="0.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA644221" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="2.9" l="1.3" alpha_wt="4.0" phi="33.0" dihedral="0.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="STCYR172" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="5.8" l="0.8" alpha_wt="3.0" phi="33.0" dihedral="0.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="STCYR172" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="5.85" l="0.8" alpha_wt="3.0" phi="33.0" dihedral="15.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="STCYR172" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="5.927" l="0.8" alpha_wt="4.0" phi="33.0" dihedral="45.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="STCYR172" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="6.005" l="0.8" alpha_wt="4.0" phi="33.0" dihedral="75.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="STCYR172" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="6.08" l="0.8" alpha_wt="4.0" phi="45.0" dihedral="95.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA0021" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="8.18" l="0.5" alpha_wt="0.0" phi="45.0" dihedral="105.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA0021" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="8.26" l="0.5" alpha_wt="0.0" phi="45.0" dihedral="135.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA0021" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="8.338" l="0.5" alpha_wt="0.0" phi="10.0" dihedral="165.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA0015" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="8.45" l="0.7" alpha_wt="0.0" phi="10.0" dihedral="180.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA0015" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="8.6" l="0.7" alpha_wt="0.0" phi="10.0" dihedral="180.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA0015" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="8.65" l="0.7" alpha_wt="0.0" phi="10.0" dihedral="180.0" flapchord="0.2" flapdeflection="20.0"/>
                        <Airfoil name="NACA0015" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="9.75" l="0.5" alpha_wt="0.0" phi="10.0" dihedral="180.0" flapchord="0.2" flapdeflection="20.0"/>
                        <Airfoil name="NACA0015" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="9.8" l="0.5" alpha_wt="0.0" phi="10.0" dihedral="180.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA0015" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="10.0" l="0.5" alpha_wt="-0.0" phi="0.0" dihedral="260.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="N64008A" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="10.3" l="0.2" alpha_wt="0.0" phi="0.0" dihedral="0.0" flapchord="0.2" flapdeflection="0.0"/>
                    </Airfoils>
                </Geometry>
                <Discretization npwingstrip="48">
                    <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"/>
                    <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="4" aoa="-3.0 5.0 10.0 " nsubpanels="15" normalizedzetaoffset="0.005" wakelength="1000.0" normalizedfarfield="5.0"/>
        <Optimization enabled="false">
            <GoalType goalType="maximize"/>
            <ObjectiveFunction objective="currentE"/>
            <Optimizer algorithm="BOBYQA" maxEvaluations="1000"/>
        </Optimization>
        <ParamaterStudies enabled="false" nsteps="20">
            <ObjectiveFunction objective="currentE"/>
        </ParamaterStudies>
    </Model>
</AeolusASP>