<?xml version="1.0"?>
<!--
  File:     CFM56_5B4.xml
  Author:   Aero-Matic v 0.81

  Inputs:
    name:           CFM56_5B4
    type:           turbine
    thrust:         27000 lb
    augmented?      no
    injected?       no
-->

<turbine_engine name="CFM56_5B4">
  <milthrust>     27000 </milthrust>
  <bypassratio>     7.1 </bypassratio>
  <tsfc>            0.8 </tsfc>
  <bleed>          0.03 </bleed>
  <idlen1>         23.4 </idlen1>
  <idlen2>         63.7 </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  0.1700
     1.0   1.3690  1.1200  0.8710  0.6510  0.4750  0.3150  0.1950
     1.2   1.4850  1.2300  0.9750  0.7440  0.5450  0.3640  0.2250
     1.4   1.5941  1.3400  1.0860  0.8450  0.6280  0.4240  0.2630
    </tableData>
   </table>
  </function>

</turbine_engine>