<?xml version="1.0" encoding="UTF-8"?>
<AeolusASP>
    <Info version="4.14" timestamp="06/09/2020 20:19:36"/>
    <Model type="aircraft">
        <UnitSystem type="si10"/>
        <Wings>
            <Wing name="Main wing" color="0.0 0.6000000238418579 0.800000011920929">
                <Geometry origin="3.0 0.0 1.0" epsilon_ref="0.25">
                    <Settings chordMode="0"/>
                    <Airfoils>
                        <Airfoil name="NACA63612" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.0" l="1.8" alpha_wt="-0.0" phi="12.0" dihedral="3.0" flapchord="0.2" flapdeflection="0.0"/>
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                        <Airfoil name="NACA63612" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="4.676778536889779" l="0.62" alpha_wt="-0.0" phi="20.0" dihedral="29.099999999999998" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA63612" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="4.828039357136999" l="0.54" alpha_wt="-0.0" phi="20.0" dihedral="46.5" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA63612" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="4.979300177384218" l="0.45999999999999996" alpha_wt="-0.0" phi="20.0" dihedral="63.9" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA63612" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="5.130560997631437" l="0.38" alpha_wt="-0.0" phi="22.0" dihedral="81.3" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA63612" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="5.281821817878656" l="0.30000000000000004" alpha_wt="-0.0" phi="24.0" dihedral="90.0" flapchord="0.2" flapdeflection="0.0"/>
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                    </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"/>
                </Discretization>
            </Wing>
            <Wing name="Flap" color="0.800000011920929 0.4000000059604645 0.0">
                <Geometry origin="4.4 0.0 0.9" epsilon_ref="0.25">
                    <Settings chordMode="0"/>
                    <Airfoils>
                        <Airfoil name="USA35A" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.4" l="0.5" alpha_wt="15.0" phi="2.2" dihedral="4.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="USA35A" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="3.0" l="0.3" alpha_wt="15.0" phi="0.0" dihedral="0.0" flapchord="0.2" flapdeflection="0.0"/>
                    </Airfoils>
                </Geometry>
                <Discretization npwingstrip="48">
                    <Strip stripdensity="0.2" type="Both"/>
                </Discretization>
            </Wing>
            <Wing name="HTP" color="0.6000000238418579 0.0 0.6000000238418579">
                <Geometry origin="7.0 0.0 3.0" epsilon_ref="0.0">
                    <Settings chordMode="0"/>
                    <Airfoils>
                        <Airfoil name="NACA0015" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.0" l="0.8" alpha_wt="-0.0" phi="20.0" dihedral="0.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="NACA0012" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.8" l="0.4" 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="Outboard"/>
                </Discretization>
            </Wing>
            <Wing name="Nacelle" color="0.800000011920929 0.800000011920929 0.0">
                <Geometry origin="4.0 1.0 2.0" epsilon_ref="0.25">
                    <Settings chordMode="0"/>
                    <Airfoils>
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                        <Airfoil name="GOE419" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.3637241502108355" l="1.5" alpha_wt="-0.0" phi="0.0" dihedral="-315.00000000000017" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="GOE419" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.384386637335242" l="1.5" alpha_wt="-0.0" phi="0.0" dihedral="-319.73684210526335" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="GOE419" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.4050491244596486" l="1.5" alpha_wt="-0.0" phi="0.0" dihedral="-324.4736842105265" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="GOE419" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.4257116115840551" l="1.5" alpha_wt="-0.0" phi="0.0" dihedral="-329.2105263157897" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="GOE419" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.4463740987084617" l="1.5" alpha_wt="-0.0" phi="0.0" dihedral="-333.9473684210529" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="GOE419" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.4670365858328682" l="1.5" alpha_wt="-0.0" phi="0.0" dihedral="-338.68421052631606" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="GOE419" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.4876990729572748" l="1.5" alpha_wt="-0.0" phi="0.0" dihedral="-343.42105263157924" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="GOE419" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.5083615600816813" l="1.5" alpha_wt="-0.0" phi="0.0" dihedral="-348.1578947368424" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="GOE419" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.5290240472060879" l="1.5" alpha_wt="-0.0" phi="0.0" dihedral="-352.8947368421056" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="GOE419" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.5496865343304944" l="1.5" alpha_wt="-0.0" phi="0.0" dihedral="0.0" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="GOE419" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.570349021454902" l="1.5" 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"/>
                    <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"/>
                    <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"/>
                    <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"/>
                    <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="45000.0" fluid="air" altitude="2000.0" temperature="15.0" trueSpeed="75.0" 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>