<?xml version="1.0" encoding="utf-8"?>
<cpacs>
  <vehicles uID="AGILE_DC1_vehicleID">
    <aircraft>
      <model uID="agile_v13_modelID">
        <wings>
          <wing symmetry="x-z-plane" uID="MainWing_wingID">
            <parentUID>Fuselage_fuselageID</parentUID>
            <sections>
              <section uID="MainWing_wingSection1ID">
                <name>MainWingSection1</name>
                <transformation>
                  <scaling>
                    <x>1</x>
                    <y>1</y>
                    <z>1</z>
                  </scaling>
                  <rotation>
                    <x>0</x>
                    <y>0</y>
                    <z>0</z>
                  </rotation>
                  <translation refType="absLocal">
                    <x>0</x>
                    <y>0</y>
                    <z>0</z>
                  </translation>
                </transformation>
                <elements>
                  <element uID="MainWing_wingSection1Element1ID">
                    <name>MainWingSection1</name>
                    <airfoilUID>Profile_MainWing_1ID</airfoilUID>
                    <transformation>
                      <scaling>
                        <x>6.3923</x>
                        <y>6.3923</y>
                        <z>6.3923</z>
                      </scaling>
                      <rotation>
                        <x>0</x>
                        <y>0</y>
                        <z>0</z>
                      </rotation>
                      <translation refType="absLocal">
                        <x>0</x>
                        <y>0</y>
                        <z>0</z>
                      </translation>
                    </transformation>
                  </element>
                </elements>
              </section>
              <section uID="MainWing_wingSection2ID">
                <name>MainWingSection2</name>
                <transformation>
                  <scaling>
                    <x>1</x>
                    <y>1</y>
                    <z>1</z>
                  </scaling>
                  <rotation>
                    <x>0</x>
                    <y>0</y>
                    <z>0</z>
                  </rotation>
                  <translation refType="absLocal">
                    <x>0</x>
                    <y>0</y>
                    <z>0</z>
                  </translation>
                </transformation>
                <elements>
                  <element uID="MainWing_wingSection2Element1ID">
                    <name>MainWingSection2</name>
                    <airfoilUID>Profile_MainWing_2ID</airfoilUID>
                    <transformation>
                      <scaling>
                        <x>2.71737</x>
                        <y>2.71737</y>
                        <z>2.71737</z>
                      </scaling>
                      <rotation>
                        <x>0</x>
                        <y>0</y>
                        <z>0</z>
                      </rotation>
                      <translation refType="absLocal">
                        <x>0</x>
                        <y>0</y>
                        <z>0</z>
                      </translation>
                    </transformation>
                  </element>
                </elements>
              </section>
              <section uID="MainWing_wingSection3ID">
                <name>MainWingSection3</name>
                <transformation>
                  <scaling>
                    <x>1</x>
                    <y>1</y>
                    <z>1</z>
                  </scaling>
                  <rotation>
                    <x>0</x>
                    <y>0</y>
                    <z>0</z>
                  </rotation>
                  <translation refType="absLocal">
                    <x>0</x>
                    <y>0</y>
                    <z>0</z>
                  </translation>
                </transformation>
                <elements>
                  <element uID="MainWing_wingSection3Element1ID">
                    <name>MainWingSection3</name>
                    <airfoilUID>Profile_MainWing_3ID</airfoilUID>
                    <transformation>
                      <scaling>
                        <x>1.05165</x>
                        <y>1.05165</y>
                        <z>1.05165</z>
                      </scaling>
                      <rotation>
                        <x>0</x>
                        <y>0</y>
                        <z>0</z>
                      </rotation>
                      <translation refType="absLocal">
                        <x>0</x>
                        <y>0</y>
                        <z>0</z>
                      </translation>
                    </transformation>
                  </element>
                </elements>
              </section>
            </sections>
            <positionings>
              <positioning uID="MainWing_wingPositioning1ID">
                <name>MainWingPositioning1</name>
                <length>0</length>
                <sweepAngle>0</sweepAngle>
                <dihedralAngle>0</dihedralAngle>
                <toSectionUID>MainWing_wingSection1ID</toSectionUID>
              </positioning>
              <positioning uID="MainWing_wingPositioning2ID">
                <name>MainWingPositioning2</name>
                <length>6.73236</length>
                <sweepAngle>33.2273</sweepAngle>
                <dihedralAngle>6</dihedralAngle>
                <fromSectionUID>MainWing_wingSection1ID</fromSectionUID>
                <toSectionUID>MainWing_wingSection2ID</toSectionUID>
              </positioning>
              <positioning uID="MainWing_wingPositioning3ID">
                <name>MainWingPositioning3</name>
                <length>9.60746</length>
                <sweepAngle>28.4037</sweepAngle>
                <dihedralAngle>6</dihedralAngle>
                <fromSectionUID>MainWing_wingSection2ID</fromSectionUID>
                <toSectionUID>MainWing_wingSection3ID</toSectionUID>
              </positioning>
            </positionings>
            <segments>
              <segment uID="MainWing_wingSegment1ID">
                <name>MainWingSegment1</name>
                <fromElementUID>MainWing_wingSection1Element1ID</fromElementUID>
                <toElementUID>MainWing_wingSection2Element1ID</toElementUID>
              </segment>
              <segment uID="MainWing_wingSegment2ID">
                <name>MainWingSegment2</name>
                <fromElementUID>MainWing_wingSection2Element1ID</fromElementUID>
                <toElementUID>MainWing_wingSection3Element1ID</toElementUID>
              </segment>
            </segments>
            <componentSegments>
              <componentSegment uID="wing_Cseg">
                <structure>
                  <upperShell uID="">
                    <skin>
                      <material>
                        <materialUID isLink="True">aluminium7075</materialUID>
                        <thickness>0.003</thickness>
                      </material>
                    </skin>
                    <stringer>
                      <stringerStructureUID isLink="True">Stringer_WING_up</stringerStructureUID>
                      <pitch>0.14</pitch>
                      <angle>0.0</angle>
                    </stringer>
                  </upperShell>
                  <ribsDefinitions>
                    <ribsDefinition uID="wing_ribs_inner">
                      <name>wing_ribs</name>
                      <ribsPositioning>
                        <ribReference>frontSpar</ribReference>
                        <etaStart>0.0</etaStart>
                        <etaEnd>0.106761565836</etaEnd>
                        <ribStart>frontSpar</ribStart>
                        <ribEnd>rearSpar</ribEnd>
                        <numberOfRibs>4</numberOfRibs>
                        <ribCrossingBehaviour>cross</ribCrossingBehaviour>
                        <ribRotation>
                          <ribRotationReference>globalY</ribRotationReference>
                          <z>90.</z>
                        </ribRotation>
                      </ribsPositioning>
                      <ribCrossSection>
                        <material>
                          <materialUID isLink="True">aluminium7075</materialUID>
                          <thickness>0.03</thickness>
                        </material>
                      </ribCrossSection>
                    </ribsDefinition>
                    <ribsDefinition uID="wing_ribs_engine1">
                      <name>wing_ribs</name>
                      <ribsPositioning>
                        <ribReference>frontSpar</ribReference>
                        <etaStart>0.163701067616</etaStart>
                        <etaEnd>0.286476868327</etaEnd>
                        <ribStart>frontSpar</ribStart>
                        <ribEnd>rearSpar</ribEnd>
                        <numberOfRibs>3</numberOfRibs>
                        <ribCrossingBehaviour>cross</ribCrossingBehaviour>
                        <ribRotation>
                          <ribRotationReference>globalY</ribRotationReference>
                          <z>90.</z>
                        </ribRotation>
                      </ribsPositioning>
                      <ribCrossSection>
                        <material>
                          <materialUID isLink="True">aluminium7075</materialUID>
                          <thickness>0.03</thickness>
                        </material>
                      </ribCrossSection>
                    </ribsDefinition>
                    <ribsDefinition uID="wing_ribs_engine2">
                      <name>wing_ribs</name>
                      <ribsPositioning>
                        <ribReference>frontSpar</ribReference>
                        <etaStart>0.163701067616</etaStart>
                        <etaEnd>0.313523131673</etaEnd>
                        <ribStart>frontSpar</ribStart>
                        <ribEnd>rearSpar</ribEnd>
                        <numberOfRibs>1</numberOfRibs>
                        <ribCrossingBehaviour>cross</ribCrossingBehaviour>
                        <ribRotation>
                          <ribRotationReference>globalY</ribRotationReference>
                          <z>90.</z>
                        </ribRotation>
                      </ribsPositioning>
                      <ribCrossSection>
                        <material>
                          <materialUID isLink="True">aluminium7075</materialUID>
                          <thickness>0.03</thickness>
                        </material>
                      </ribCrossSection>
                    </ribsDefinition>
                    <ribsDefinition uID="wing_ribs_outer">
                      <name>wing_ribs</name>
                      <ribsPositioning>
                        <ribReference>frontSpar</ribReference>
                        <etaStart>0.370462633452</etaStart>
                        <etaEnd>0.95</etaEnd>
                        <ribStart>frontSpar</ribStart>
                        <ribEnd>rearSpar</ribEnd>
                        <numberOfRibs>11</numberOfRibs>
                        <ribCrossingBehaviour>end</ribCrossingBehaviour>
                        <ribRotation>
                          <ribRotationReference>frontSpar</ribRotationReference>
                          <z>90.</z>
                        </ribRotation>
                      </ribsPositioning>
                      <ribCrossSection>
                        <material>
                          <materialUID isLink="True">aluminium7075</materialUID>
                          <thickness>0.03</thickness>
                        </material>
                      </ribCrossSection>
                    </ribsDefinition>
                  </ribsDefinitions>
                  <spars>
                    <sparPositions>
                      <sparPosition uID="frontSpar_P0">
                        <eta>0.0</eta>
                        <xsi>0.1</xsi>
                      </sparPosition>
                      <sparPosition uID="frontSpar_P1">
                        <eta>0.106761565836</eta>
                        <xsi>0.1</xsi>
                      </sparPosition>
                      <sparPosition uID="frontSpar_P2">
                        <eta>1.0</eta>
                        <xsi>0.460829493088</xsi>
                      </sparPosition>
                      <sparPosition uID="rearSpar_P0">
                        <eta>0.0</eta>
                        <xsi>0.56</xsi>
                      </sparPosition>
                      <sparPosition uID="rearSpar_P1">
                        <eta>0.106761565836</eta>
                        <xsi>0.56</xsi>
                      </sparPosition>
                      <sparPosition uID="rearSpar_P2">
                        <eta>0.350213340505</eta>
                        <xsi>0.6</xsi>
                      </sparPosition>
                      <sparPosition uID="rearSpar_P3">
                        <eta>1.0</eta>
                        <xsi>0.59</xsi>
                      </sparPosition>
                    </sparPositions>
                    <sparSegments>
                      <sparSegment uID="frontSpar">
                        <name>frontSpar</name>
                        <description>frontSpar</description>
                        <sparPositionUIDs>
                          <sparPositionUID isLink="True">frontSpar_P0</sparPositionUID>
                          <sparPositionUID isLink="True">frontSpar_P1</sparPositionUID>
                          <sparPositionUID isLink="True">frontSpar_P2</sparPositionUID>
                        </sparPositionUIDs>
                        <sparCrossSection>
                          <upperCap>
                            <area>0.0003</area>
                            <material>
                              <materialUID isLink="True">aluminium7075</materialUID>
                              <thickness>0.003</thickness>
                            </material>
                          </upperCap>
                          <lowerCap>
                            <area>0.0003</area>
                            <material>
                              <materialUID isLink="True">aluminium7075</materialUID>
                              <thickness>0.003</thickness>
                            </material>
                          </lowerCap>
                          <web1>
                            <material>
                              <materialUID isLink="True">aluminium7075</materialUID>
                              <thickness>0.003</thickness>
                            </material>
                            <relPos>0.5</relPos>
                          </web1>
                          <rotation>90.0</rotation>
                        </sparCrossSection>
                      </sparSegment>
                      <sparSegment uID="rearSpar">
                        <name>rearSpar</name>
                        <description>rearSpar</description>
                        <sparPositionUIDs>
                          <sparPositionUID isLink="True">rearSpar_P0</sparPositionUID>
                          <sparPositionUID isLink="True">rearSpar_P1</sparPositionUID>
                          <sparPositionUID isLink="True">rearSpar_P2</sparPositionUID>
                          <sparPositionUID isLink="True">rearSpar_P3</sparPositionUID>
                        </sparPositionUIDs>
                        <sparCrossSection>
                          <upperCap>
                            <area>0.0003</area>
                            <material>
                              <materialUID isLink="True">aluminium7075</materialUID>
                              <thickness>0.003</thickness>
                            </material>
                          </upperCap>
                          <lowerCap>
                            <area>0.0003</area>
                            <material>
                              <materialUID isLink="True">aluminium7075</materialUID>
                              <thickness>0.003</thickness>
                            </material>
                          </lowerCap>
                          <web1>
                            <material>
                              <materialUID isLink="True">aluminium7075</materialUID>
                              <thickness>0.003</thickness>
                            </material>
                            <relPos>0.5</relPos>
                          </web1>
                          <rotation>90.0</rotation>
                        </sparCrossSection>
                      </sparSegment>
                    </sparSegments>
                  </spars>
                </structure>
              </componentSegment>
            </componentSegments>
          </wing>
        </wings>
        <analyses>
          <loadAnalysis>
            <loadCases>
              <aeroDataSetsForLoads>
                <aeroDataSetForLoads uID="Design-maneuver-speed_2.5g_F0_MTOM_max_fuel_12000m_aeroDataSet">
                  <flowCondition>
                    <machNumber>0.78</machNumber>
                    <reynoldsNumber>18792419.4249</reynoldsNumber>
                    <angleOfYaw>0.0</angleOfYaw>
                    <targetLiftCoefficient>1.1096</targetLiftCoefficient>
                  </flowCondition>
                  <wings>
                    <wing>
                      <wingUID>MainWing_wingID</wingUID>
                      <coefficients>
                        <cfz>1.1096</cfz>
                        <cmy>-1.4781</cmy>
                      </coefficients>
                      <segments>
                        <segment>
                          <strip>
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                            <reference>
                              <length>6.1626</length>
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                                <y>0.3500</y>
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                          </strip>
                          <strip>
                            <cfz>0.8129</cfz>
                            <cmy>-0.1447</cmy>
                            <reference>
                              <length>5.7033</length>
                              <flightShapePoint>
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                                <y>1.0501</y>
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                          </strip>
                          <strip>
                            <cfz>0.8675</cfz>
                            <cmy>-0.1414</cmy>
                            <reference>
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                          <strip>
                            <cfz>0.9256</cfz>
                            <cmy>-0.1389</cmy>
                            <reference>
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                          <strip>
                            <cfz>0.989</cfz>
                            <cmy>-0.1368</cmy>
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                              <length>4.3252</length>
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                          </strip>
                          <strip>
                            <cfz>1.06</cfz>
                            <cmy>-0.1349</cmy>
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                              <length>3.8658</length>
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                            <cfz>1.1422</cfz>
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                              <length>2.9471</length>
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                          </strip>
                          <segmentUID>MainWing_wingSegment1ID</segmentUID>
                        </segment>
                        <segment>
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                            <reference>
                              <length>2.648</length>
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                            <cfz>1.3416</cfz>
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                            <cfz>1.3656</cfz>
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                              <length>2.0927</length>
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                                <x>18.2024</x>
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                            <cfz>1.4162</cfz>
                            <cmy>-0.1056</cmy>
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                              <length>1.9539</length>
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                                <y>9.4529</y>
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                          <strip>
                            <cfz>1.4411</cfz>
                            <cmy>-0.1074</cmy>
                            <reference>
                              <length>1.8151</length>
                              <flightShapePoint>
                                <x>18.8994</x>
                                <y>10.1533</y>
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                            </reference>
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                          <strip>
                            <cfz>1.4635</cfz>
                            <cmy>-0.1091</cmy>
                            <reference>
                              <length>1.6763</length>
                              <flightShapePoint>
                                <x>19.2479</x>
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                          <strip>
                            <cfz>1.479</cfz>
                            <cmy>-0.1102</cmy>
                            <reference>
                              <length>1.5375</length>
                              <flightShapePoint>
                                <x>19.5964</x>
                                <y>11.5541</y>
                                <z>0.0585</z>
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                            </reference>
                          </strip>
                          <strip>
                            <cfz>1.476</cfz>
                            <cmy>-0.1087</cmy>
                            <reference>
                              <length>1.3987</length>
                              <flightShapePoint>
                                <x>19.9449</x>
                                <y>12.2544</y>
                                <z>0.1200</z>
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                            </reference>
                          </strip>
                          <strip>
                            <cfz>1.4208</cfz>
                            <cmy>-0.0998</cmy>
                            <reference>
                              <length>1.2599</length>
                              <flightShapePoint>
                                <x>20.2934</x>
                                <y>12.9548</y>
                                <z>0.1814</z>
                              </flightShapePoint>
                            </reference>
                          </strip>
                          <strip>
                            <cfz>1.194</cfz>
                            <cmy>-0.0721</cmy>
                            <reference>
                              <length>1.1211</length>
                              <flightShapePoint>
                                <x>20.6419</x>
                                <y>13.6552</y>
                                <z>0.2429</z>
                              </flightShapePoint>
                            </reference>
                          </strip>
                          <segmentUID>MainWing_wingSegment2ID</segmentUID>
                        </segment>
                      </segments>
                    </wing>
                  </wings>
                </aeroDataSetForLoads>
              </aeroDataSetsForLoads>
              <flightLoadCases>
                <flightLoadCase uID="Design-maneuver-speed_2.5g_F0_MTOM_max_fuel_12000m">
                  <aeroDataSetUID>Design-maneuver-speed_2.5g_F0_MTOM_max_fuel_12000m_aeroDataSet</aeroDataSetUID>
                  <state>
                    <atmosphericConditions>
                      <density>0.31093</density>
                      <temperature>216.5839</temperature>
                      <speedOfSound>295.1</speedOfSound>
                    </atmosphericConditions>
                    <attitudeAndMotion>
                      <refPointUID>refPointUID</refPointUID>
                      <refRotation>
                        <x>0.0</x>
                        <y>0.0</y>
                        <z>0.0</z>
                      </refRotation>
                      <translation>
                        <velocity>
                          <u>230.178</u>
                        </velocity>
                        <acceleration>
                          <wDot>14.715</wDot>
                        </acceleration>
                      </translation>
                    </attitudeAndMotion>
                  </state>
                  <mass>
                    <weightAndBalanceUID>MTOW1</weightAndBalanceUID>
                  </mass>
                </flightLoadCase>
              </flightLoadCases>
            </loadCases>
          </loadAnalysis>
        </analyses>
      </model>
    </aircraft>
    <materials>
      <material uID="aluminium2024">
        <rho>2.8e3</rho>
        <k11>80.9561216474e9</k11>
        <sig11>0.3268e9</sig11>
      </material>
      <material uID="aluminium7075">
        <rho>2.8e3</rho>
        <k11>80.9561216474e9</k11>
        <sig11>0.3268e9</sig11>
      </material>
    </materials>
  </vehicles>
  <toolspecific>
    <proteus>
      <inputData>
        <wingUID>MainWing_wingID</wingUID>
        <beamElements>8</beamElements>
        <spanwisePanels>12</spanwisePanels>
        <chordwisePanels>10</chordwisePanels>
        <crosssectionalElements>75</crosssectionalElements>
        <linear>1</linear>
        <trim>1</trim>
        <weightDefinition>1</weightDefinition>
        <gravity>1</gravity>
        <graphic>0</graphic>
      </inputData>
    </proteus>
  </toolspecific>
</cpacs>
