<?xml version="1.0"?>
<!--
  File:     Trent-900.xml
  Author:   Aero-Matic v 0.8

  Inputs:
    name:           Trent-900
    type:           turbine
    thrust:         80000 lb
    augmented?      no
    injected?       no
-->

<turbine_engine name="TRENT-900">
  <milthrust> 80000 </milthrust>
  <bypassratio>    8.0 </bypassratio>
  <tsfc>           0.5 </tsfc>
  <idlen1>        20.0 </idlen1>
  <idlen2>        60.0 </idlen2>
  <maxn1>        100.0 </maxn1>
  <maxn2>        100.0 </maxn2>
  <augmented>      0 </augmented>
  <augmethod>      1 </augmethod>
  <injected>       0 </injected>
  
 <function name="IdleThrust">
  <table>
   <independentVar lookup="row">velocities/mach</independentVar>
   <independentVar lookup="column">position/h-sl-ft</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     0.0     0.0276  0.0718  0.1073  0.0
    0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900  0.0
    1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800  0.0
   </tableData>
  </table>
 </function>

 <function name="MilThrust">
  <table>
   <independentVar lookup="row">velocities/mach</independentVar>
   <independentVar lookup="column">position/h-sl-ft</independentVar>
   <tableData>
          -10000       0   10000   20000   30000   40000   50000  60000
    0.0   1.2600  1.0000  0.7400  0.5340  0.3720  0.2410  0.1490  0.0
    0.2   1.1710  0.9340  0.6970  0.5060  0.3550  0.2310  0.1430  0.0
    0.4   1.1500  0.9210  0.6920  0.5060  0.3570  0.2330  0.1450  0.0
    0.6   1.1810  0.9510  0.7210  0.5320  0.3780  0.2480  0.1540  0.0
    0.8   1.2580  1.0200  0.7820  0.5820  0.4170  0.2750  0.1700  0.0
    1.0   1.3690  1.1200  0.8710  0.6510  0.4750  0.3150  0.1950  0.0
    1.2   1.4850  1.2300  0.9750  0.7440  0.5450  0.3640  0.2250  0.0
    1.4   1.5941  1.3400  1.0860  0.8450  0.6280  0.4240  0.2630  0.0
   </tableData>
  </table>
 </function>

</turbine_engine>
