<?xml version="1.0" encoding="UTF-8"?>
<AeolusASP>
    <Info version="4.25" timestamp="03/09/2022 16:51:16"/>
    <Model type="aircraft" name="Paraglider">
        <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="0.95" scale="1.0">
                    <Settings chordMode="0"/>
                    <Airfoils>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.0" l="2.2" alpha_wt="2.0" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="0.5" l="2.2" alpha_wt="2.0" phi="0.0" dihedral="-2.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.0" l="2.18" alpha_wt="1.0" phi="0.0" dihedral="-6.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="1.5" l="2.15" alpha_wt="0.5" phi="0.0" dihedral="-10.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="2.0" l="2.08" alpha_wt="0.0" phi="0.0" dihedral="-14.0" inverted="false" flapchord="0.2" flapdeflection="0.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="2.5" l="2.0" alpha_wt="0.0" phi="0.0" dihedral="-18.0" inverted="false" flapchord="0.2" flapdeflection="10.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="3.0" l="1.9" alpha_wt="0.0" phi="0.0" dihedral="-24.0" inverted="false" flapchord="0.2" flapdeflection="20.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="3.5" l="1.78" alpha_wt="0.0" phi="0.0" dihedral="-28.0" inverted="false" flapchord="0.2" flapdeflection="20.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="4.0" l="1.65" alpha_wt="0.0" phi="0.0" dihedral="-31.0" inverted="false" flapchord="0.2" flapdeflection="20.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="4.5" l="1.5" alpha_wt="0.0" phi="0.0" dihedral="-38.0" inverted="false" flapchord="0.2" flapdeflection="20.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="4.75" l="1.4" alpha_wt="0.0" phi="0.0" dihedral="-45.0" inverted="false" flapchord="0.2" flapdeflection="20.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="5.0" l="1.3" alpha_wt="1.0" phi="0.0" dihedral="-52.0" inverted="false" flapchord="0.2" flapdeflection="20.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="5.5" l="1.04" alpha_wt="2.0" phi="0.0" dihedral="-65.0" inverted="false" flapchord="0.2" flapdeflection="20.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="5.825" l="0.8" alpha_wt="4.0" phi="0.0" dihedral="-70.0" inverted="false" flapchord="0.2" flapdeflection="20.0"/>
                        <Airfoil name="LS416MOD-IL" refinement="0.9" refinementSourceTop="0.6" refinementSourceBot="0.6" s="6.15" l="0.4" alpha_wt="5.0" phi="0.0" dihedral="0.0" inverted="false" flapchord="0.2" flapdeflection="20.0"/>
                    </Airfoils>
                </Geometry>
                <Discretization smooth="true" npwingstrip="58">
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                    <Strip stripdensity="0.5" type="Constant"/>
                </Discretization>
            </Wing>
        </Wings>
        <Propulsion>
        </Propulsion>
        <FlightCondition aircraftWeight="833.0" fluid="air" altitude="2000.0" temperature="15.0" trueSpeed="10.0" 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="false">
            <GoalType goalType="maximize"/>
            <ObjectiveFunction objective="currentE"/>
            <Optimizer algorithm="BOBYQA" maxEvaluations="1000"/>
        </Optimization>
        <ParamaterStudies enabled="false" nsteps="20">
            <ObjectiveFunction objective="currentE"/>
        </ParamaterStudies>
    </Model>
</AeolusASP>