airoptserver/src/main/resources/templates/cpacs.ftl

<cpacs xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="../schema/cpacs_schema.xsd">
    <header>
        <name>${vo.header.name}</name>
        <creator>SurroMDAO</creator>
        <timestamp>${vo.header.timestamp}</timestamp>
        <version>1.0</version>
        <cpacsVersion>3.3</cpacsVersion>
    </header>
    <vehicles>
        <#if vo.cst??>
        <profiles>
            <wingAirfoils>
                <wingAirfoil uID="foil1">
                    <name>foil1</name>
                    <description>airfoil</description>
                    <cst2D mapType="complex">
                        <N>${vo.cst.cstn}</N>
                        <lowerB mapType="vector">${vo.cst.lowerb?replace( ",", ";")}</lowerB>
                        <lowerN1 mapType="dobule">${vo.cst.lowern1}</lowerN1>
                        <lowerN2 mapType="dobule">${vo.cst.lowern2}</lowerN2>
                        <upperB mapType="vector">${vo.cst.upperb?replace(",", ";")}</upperB>
                        <upperN1 mapType="dobule">${vo.cst.uppern1}</upperN1>
                        <upperN2 mapType="dobule">${vo.cst.uppern2}</upperN2>
                        <trailingEdgeThickness mapType="dobule">0</trailingEdgeThickness>
                    </cst2D>
                </wingAirfoil>
            </wingAirfoils>
        </profiles>
        <#else>
        </#if>
        <#if vo.adflow??>
        <aircraft>
            <model uID="wing">
                <name>wing</name>
                <reference mapType="complex">
                    <area mapType="double">${vo.adflow.area}</area>
                    <length mapType="double">${vo.adflow.length}</length>
                    <point mapType="complex">
                        <x mapType="double">${vo.adflow.momx}</x>
                        <y mapType="double">${vo.adflow.momy}</y>
                        <z mapType="double">${vo.adflow.momz}</z>
                    </point>
                </reference>
            </model>
        </aircraft>
        <#else>
        </#if>
    </vehicles>
    <toolspecific>
       <#if vo.ffd??>
         <FFD mapType="complex" uID="FFD">
                <switch mapType="boolean">1</switch>
                <FFDFile>${vo.ffd.fname}</FFDFile>
                <order mapType="integer">${vo.ffd.fname}</order>
                <Controlpoints mapType="complex">
                    <Nx mapType="integer">${vo.ffd.nx}</Nx>
                    <Ny mapType="integer">${vo.ffd.ny}</Ny>
                    <Nz mapType="integer">${vo.ffd.nz}</Nz>
                </Controlpoints>
                <vars mapType="complex">
                    <sample mapType="vector">${vo.ffd.vars?replace( ",", ";")}</sample>
                    <local_shape_dv mapType="boolean">1</local_shape_dv>
                </vars>
         </FFD>
      <#else>
      </#if>
        <CFD>
         <#if vo.xfoil??>
            <XFOIL mapType="complex" uID="XFOIL">
                <analyzed mapType="boolean">1</analyzed>
                <options mapType="complex">
                    <pacc>${vo.xfoil.pacc}</pacc>
                    <cpwr>${vo.xfoil.cpwr}</cpwr>
                    <iter mapType="integer">${vo.xfoil.iter}</iter>
                    <ppar mapType="integer">${vo.xfoil.ppar}</ppar>
                </options>
                <condition mapType="complex">
                    <alpha mapType="double">${vo.xinvo.alpha}</alpha>
                    <mach mapType="double">${vo.xinvo.mach}</mach>
                    <reynolds mapType="double">${vo.xinvo.reynolds}</reynolds>
                </condition>
                <evalFuncs mapType="complex">
                    <cl mapType="double">${vo.xoutvo.cl}</cl>
                    <cd mapType="double">${vo.xoutvo.cd}</cd>
                    <cdp mapType="double">${vo.xoutvo.cdp}</cdp>
                    <cm mapType="double">${vo.xoutvo.cm}</cm>
                    <xtr_upper mapType="double">${vo.xoutvo.xtr_upper}</xtr_upper>
                    <xtr_lower mapType="double">${vo.xoutvo.xtr_lower}</xtr_lower>
                </evalFuncs>
            </XFOIL>
         <#else>
         </#if>
         <#if vo.adflow??>
             <ADflow mapType="complex" uID="ADflow">
             <switch mapType="boolean">1</switch>
             <proName>${vo.adflow.proname}</proName>
             <analyzed mapType="boolean">0</analyzed>
             <isAirfoil mapType="boolean">${vo.adflow.isairfoil}</isAirfoil>
             <inputDirectoryName>model</inputDirectoryName>
             <outputDirectoryName>results</outputDirectoryName>
             <options mapType="complex">
                 <gridFile>${vo.adflow.gridfile}</gridFile>
                 <writeTecplotSurfaceSolution mapType="boolean">${vo.adflow.writetecplotsurfacesolution}</writeTecplotSurfaceSolution>
                 <equationType>${vo.adflow.equationtype}</equationType>
                 <smoother>DADI</smoother>
                 <MGCycle>${vo.adflow.mgcycle}</MGCycle>
                 <nCycles mapType="integer">${vo.adflow.ncycles}</nCycles>
                 <monitorvariables mapType="complex">
                        <#if vo.adflow.resrho?trim == "1">
                        <monitorvariable1>resrho</monitorvariable1>
                        <#else>
                        </#if>
                        <#if vo.adflow.cl?trim == "1">
                        <monitorvariable2>cl</monitorvariable2>
                        <#else>
                        </#if>
                        <#if vo.adflow.cd?trim == "1">
                        <monitorvariable2>cd</monitorvariable2>
                        <#else>
                        </#if>
                        <#if vo.adflow.cmz?trim == "1">
                        <monitorvariable2>cmz</monitorvariable2>
                        <#else>
                        </#if>
                 </monitorvariables>
                 <useNKSolver mapType="boolean">1</useNKSolver> # 使用nk求解器
                 <useanksolver mapType="boolean">1</useanksolver> # 使用ank求解器
                 <nsubiterturb mapType="integer">5</nsubiterturb>
                 <liftIndex mapType="integer">${vo.adflow.liftindex}</liftIndex>
                 <infchangecorrection mapType="boolean">1</infchangecorrection>
                 <L2Convergence mapType="double">${vo.adflow.l2convergence}</L2Convergence>
                 <L2ConvergenceCoarse mapType="double">${vo.adflow.l2convergencecoarse}</L2ConvergenceCoarse>
                 <NKSwitchTol mapType="double">1e-8</NKSwitchTol>
                 <ANKSwitchTol mapType="double">1e-1</ANKSwitchTol>
                 <L2ConvergenceRel mapType="double">1e-3</L2ConvergenceRel>
             </options>
             <condition mapType="complex">
                 <mode mapType="integer">${vo.adinvo.mode}</mode>
                 <alpha mapType="double">${vo.adinvo.alpha}</alpha>
                 <mach mapType="double">${vo.adinvo.mach}</mach>
                 <reynolds mapType="double">${vo.adinvo.reynolds}</reynolds>
                 <temperature mapType="double">${vo.adinvo.temperature}</temperature>
                 <reynoldsLength mapType="double">${vo.adinvo.reynoldsLength}</reynoldsLength>
             </condition>
             <evalFuncs mapType="complex">
                 <force mapType="complex">
                     <cl mapType="double">${vo.adoutvo.cl}</cl>
                     <cd mapType="double">${vo.adoutvo.cd}</cd>
                     <cmz mapType="double">${vo.adoutvo.cmz}</cmz>
                 </force>
                 <geometry mapType="complex">
                     <volume mapType="double">0.0</volume>
                 </geometry>
             </evalFuncs>
         </ADflow>
         <#else>
         </#if>
        </CFD>

    </toolspecific>
</cpacs>