<?xml version="1.0" encoding="UTF-8"?>
<!DOCTYPE explane>
<explane version="1.0">
    <Units>
        <length_unit_to_meter>1</length_unit_to_meter>
        <mass_unit_to_kg>1</mass_unit_to_kg>
    </Units>
    <wing>
        <Name>Sly Surfer Wing</Name>
        <Type>MAINWING</Type>
        <Color>
            <red>217</red>
            <green>126</green>
            <blue>245</blue>
            <alpha>255</alpha>
        </Color>
        <Description></Description>
        <Position>          0,           0,           0</Position>
        <Tilt_angle>  0.000</Tilt_angle>
        <Symetric>true</Symetric>
        <isFin>false</isFin>
        <isDoubleFin>false</isDoubleFin>
        <isSymFin>false</isSymFin>
        <Inertia>
            <Volume_Mass>  0.000</Volume_Mass>
        </Inertia>
        <Sections>
            <Section>
                <y_position>  0.000</y_position>
                <Chord>  0.200</Chord>
                <xOffset>  0.000</xOffset>
                <Dihedral>  0.000</Dihedral>
                <Twist>  0.000</Twist>
                <x_number_of_panels>11</x_number_of_panels>
                <x_panel_distribution>COSINE</x_panel_distribution>
                <y_number_of_panels>5</y_number_of_panels>
                <y_panel_distribution>UNIFORM</y_panel_distribution>
                <Left_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Left_Side_FoilName>
                <Right_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Right_Side_FoilName>
            </Section>
            <Section>
                <y_position>  0.180</y_position>
                <Chord>  0.200</Chord>
                <xOffset>  0.000</xOffset>
                <Dihedral>  0.000</Dihedral>
                <Twist>  0.000</Twist>
                <x_number_of_panels>11</x_number_of_panels>
                <x_panel_distribution>COSINE</x_panel_distribution>
                <y_number_of_panels>3</y_number_of_panels>
                <y_panel_distribution>UNIFORM</y_panel_distribution>
                <Left_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Left_Side_FoilName>
                <Right_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Right_Side_FoilName>
            </Section>
            <Section>
                <y_position>  0.300</y_position>
                <Chord>  0.200</Chord>
                <xOffset>  0.000</xOffset>
                <Dihedral>  0.000</Dihedral>
                <Twist>  0.000</Twist>
                <x_number_of_panels>11</x_number_of_panels>
                <x_panel_distribution>COSINE</x_panel_distribution>
                <y_number_of_panels>3</y_number_of_panels>
                <y_panel_distribution>UNIFORM</y_panel_distribution>
                <Left_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Left_Side_FoilName>
                <Right_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Right_Side_FoilName>
            </Section>
            <Section>
                <y_position>  0.420</y_position>
                <Chord>  0.178</Chord>
                <xOffset>  0.012</xOffset>
                <Dihedral>  0.000</Dihedral>
                <Twist>  0.000</Twist>
                <x_number_of_panels>11</x_number_of_panels>
                <x_panel_distribution>COSINE</x_panel_distribution>
                <y_number_of_panels>1</y_number_of_panels>
                <y_panel_distribution>UNIFORM</y_panel_distribution>
                <Left_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Left_Side_FoilName>
                <Right_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Right_Side_FoilName>
            </Section>
            <Section>
                <y_position>  0.480</y_position>
                <Chord>  0.170</Chord>
                <xOffset>  0.018</xOffset>
                <Dihedral>  6.000</Dihedral>
                <Twist>  0.000</Twist>
                <x_number_of_panels>11</x_number_of_panels>
                <x_panel_distribution>COSINE</x_panel_distribution>
                <y_number_of_panels>1</y_number_of_panels>
                <y_panel_distribution>UNIFORM</y_panel_distribution>
                <Left_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Left_Side_FoilName>
                <Right_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Right_Side_FoilName>
            </Section>
            <Section>
                <y_position>  0.540</y_position>
                <Chord>  0.155</Chord>
                <xOffset>  0.030</xOffset>
                <Dihedral> 15.000</Dihedral>
                <Twist>  0.000</Twist>
                <x_number_of_panels>11</x_number_of_panels>
                <x_panel_distribution>COSINE</x_panel_distribution>
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                <y_panel_distribution>UNIFORM</y_panel_distribution>
                <Left_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Left_Side_FoilName>
                <Right_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Right_Side_FoilName>
            </Section>
            <Section>
                <y_position>  0.580</y_position>
                <Chord>  0.140</Chord>
                <xOffset>  0.045</xOffset>
                <Dihedral> 20.000</Dihedral>
                <Twist>  0.000</Twist>
                <x_number_of_panels>11</x_number_of_panels>
                <x_panel_distribution>COSINE</x_panel_distribution>
                <y_number_of_panels>1</y_number_of_panels>
                <y_panel_distribution>UNIFORM</y_panel_distribution>
                <Left_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Left_Side_FoilName>
                <Right_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Right_Side_FoilName>
            </Section>
            <Section>
                <y_position>  0.620</y_position>
                <Chord>  0.120</Chord>
                <xOffset>  0.070</xOffset>
                <Dihedral> 22.000</Dihedral>
                <Twist>  0.000</Twist>
                <x_number_of_panels>11</x_number_of_panels>
                <x_panel_distribution>COSINE</x_panel_distribution>
                <y_number_of_panels>1</y_number_of_panels>
                <y_panel_distribution>UNIFORM</y_panel_distribution>
                <Left_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Left_Side_FoilName>
                <Right_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Right_Side_FoilName>
            </Section>
            <Section>
                <y_position>  0.660</y_position>
                <Chord>  0.095</Chord>
                <xOffset>  0.105</xOffset>
                <Dihedral> 25.000</Dihedral>
                <Twist>  0.000</Twist>
                <x_number_of_panels>11</x_number_of_panels>
                <x_panel_distribution>COSINE</x_panel_distribution>
                <y_number_of_panels>1</y_number_of_panels>
                <y_panel_distribution>UNIFORM</y_panel_distribution>
                <Left_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Left_Side_FoilName>
                <Right_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Right_Side_FoilName>
            </Section>
            <Section>
                <y_position>  0.680</y_position>
                <Chord>  0.080</Chord>
                <xOffset>  0.130</xOffset>
                <Dihedral> 27.000</Dihedral>
                <Twist>  0.000</Twist>
                <x_number_of_panels>11</x_number_of_panels>
                <x_panel_distribution>COSINE</x_panel_distribution>
                <y_number_of_panels>1</y_number_of_panels>
                <y_panel_distribution>UNIFORM</y_panel_distribution>
                <Left_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Left_Side_FoilName>
                <Right_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Right_Side_FoilName>
            </Section>
            <Section>
                <y_position>  0.690</y_position>
                <Chord>  0.060</Chord>
                <xOffset>  0.150</xOffset>
                <Dihedral> 30.000</Dihedral>
                <Twist>  0.000</Twist>
                <x_number_of_panels>11</x_number_of_panels>
                <x_panel_distribution>COSINE</x_panel_distribution>
                <y_number_of_panels>1</y_number_of_panels>
                <y_panel_distribution>UNIFORM</y_panel_distribution>
                <Left_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Left_Side_FoilName>
                <Right_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Right_Side_FoilName>
            </Section>
            <Section>
                <y_position>  0.700</y_position>
                <Chord>  0.020</Chord>
                <xOffset>  0.180</xOffset>
                <Dihedral>  0.000</Dihedral>
                <Twist>  0.000</Twist>
                <x_number_of_panels>13</x_number_of_panels>
                <x_panel_distribution>COSINE</x_panel_distribution>
                <y_number_of_panels>1</y_number_of_panels>
                <y_panel_distribution>UNIFORM</y_panel_distribution>
                <Left_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Left_Side_FoilName>
                <Right_Side_FoilName>USA 48 AIRFOIL_BLUNT TE</Right_Side_FoilName>
            </Section>
        </Sections>
    </wing>
</explane>
