<?xml version="1.0" encoding="ISO-8859-1"?>

<!--
     Test turbine for ah1/uh1, generated with aeromatic
-->

<turbine_engine name="avco_lycoming_t53_l_703">
  <milthrust> 3320 </milthrust> <!-- expect 1483 shp, via 2.24 approximated to 3320 lbf -->
  <bypassratio>     0.0  </bypassratio>
  <tsfc>            0.60 </tsfc>
  <bleed>           0.001 </bleed>
  <idlen1>         30.0  </idlen1>
  <idlen2>         60.0  </idlen2>
  <maxn1>         100.0  </maxn1>
  <maxn2>         100.0  </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     0.0276  0.0718  0.0430  0.0
     0.8  0.0     0.0     0.0     0.0     0.0174  0.0086  0.0
     1.0  0.0     0.0     0.0     0.0     0.0     0.0     0.0
   </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  1.1260  1.0000  0.7400  0.5340  0.3720  0.2410  0.1490
     0.2  1.1000  0.9340  0.6970  0.5060  0.3550  0.2310  0.1430
     0.4  1.0000  0.6410  0.6120  0.4060  0.3570  0.2330  0.1450
     0.6  0.4430  0.3510  0.2710  0.2020  0.1780  0.1020  0.0640
     0.8  0.0240  0.0200  0.0160  0.0130  0.0110  0.0100  0.0
     1.0  0.0     0.0     0.0     0.0     0.0     0.0     0.0
    </tableData>
   </table>
  </function>

</turbine_engine>
