<?xml version="1.0"?>
<!--
  File:     PW125B.xml
  Author:   Aero-Matic v 0.8

  Inputs:
    name:           PW125B
    type:           turboprop
    power:          2500 hp
    augmented?      no
    injected?       no
-->

<turbine_engine name="PW125B">
  <milthrust>    5600.00 </milthrust>
  <tsfc>            0.55 </tsfc>
  <idlen2>         60.0  </idlen2>
  <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   60000
     0.0  0.0430  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467  0.0
     0.2  0.0500  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342  0.0
     0.4  0.0040  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203  0.0
     0.6  0.0     0.0     0.0     0.0276  0.0718  0.0430  0.0     0.0
     0.8  0.0     0.0     0.0     0.0     0.0174  0.0086  0.0     0.0
     1.0  0.0     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   60000
     0.0  1.1260  1.0000  0.7400  0.5340  0.3720  0.2410  0.1490  0.0
     0.2  1.1000  0.9340  0.6970  0.5060  0.3550  0.2310  0.1430  0.0
     0.4  1.0000  0.6410  0.6120  0.4060  0.3570  0.2330  0.1450  0.0
     0.6  0.4430  0.3510  0.2710  0.2020  0.1780  0.1020  0.0640  0.0
     0.8  0.0240  0.0200  0.0160  0.0130  0.0110  0.0100  0.0     0.0
     1.0  0.0     0.0     0.0     0.0     0.0     0.0     0.0     0.0
    </tableData>
   </table>
  </function>

</turbine_engine>
