IDG-A32X/Engines/v2522_a5.xml

<?xml version="1.0"?>

<turbine_engine name="V2527_A5">
  <milthrust>     26600 </milthrust> <!-- Will put proper thrust amount once FDE sorted out -->
  <bypassratio>     7.1 </bypassratio>
  <tsfc>            0.8 </tsfc>
  <bleed>          0.03 </bleed>
  <idlen1>         22.4 </idlen1>
  <idlen2>         60.9 </idlen2>
  <n1spinup>        0.2 </n1spinup>
  <n2spinup>        2.0 </n2spinup>
  <maxn1>         105.8 </maxn1>
  <maxn2>         102.1 </maxn2>
  <augmented>         0 </augmented>
  <injected>          0 </injected>

  <function name="IdleThrust">
   <table>
    <independentVar lookup="row">velocities/mach</independentVar>
    <independentVar lookup="column">atmosphere/density-altitude</independentVar>
    <tableData>
         -10000     0     10000   20000   30000   40000   50000
     0.0  0.0430  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467
     0.2  0.0500  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342
     0.4  0.0040  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
     0.6  0.0     0.0     0.0     0.0     0.0276  0.0718  0.1073
     0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900
     1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800
    </tableData>
   </table>
  </function>

  <function name="MilThrust">
   <table>
    <independentVar lookup="row">velocities/mach</independentVar>
    <independentVar lookup="column">atmosphere/density-altitude</independentVar>
    <tableData>
          -10000       0   10000   20000   30000   40000   50000
     0.0   1.2600  1.0000  0.7400  0.5340  0.3720  0.2410  0.1490
     0.2   1.1710  0.9340  0.6970  0.5060  0.3550  0.2310  0.1430
     0.4   1.1500  0.9210  0.6920  0.5060  0.3570  0.2330  0.1450
     0.6   1.1810  0.9510  0.7210  0.5320  0.3780  0.2480  0.1540
     0.8   1.2580  1.0200  0.7820  0.5820  0.4170  0.2750  0.1600
     0.9   1.2580  1.0200  0.7820  0.5820  0.4170  0.2750  0.0000
     1.0   1.1810  0.9510  0.7210  0.5320  0.3780  0.0000  0.0000
     1.2   1.1500  0.9210  0.6920  0.0000  0.0000  0.0000  0.0000
     1.4   1.1710  0.9340  0.0000  0.0000  0.0000  0.0000  0.0000
    </tableData>
   </table>
  </function>

</turbine_engine>