jsbsim.js/JSBSim/engine/CF6-80C2.xml

JSBSim flight dynamics model ported to JavaScript

<?xml version="1.0"?>
<!--
  File:     CF6-80C2A3.xml
  Author:   Aero-Matic v 0.8, DPC

  Inputs:
    name:           CF6-80C2A3
    type:           turbine
    thrust:         60200 lb
    augmented?      no
    injected?       no

  Additional sources:
    http://www.geae.com/engines/commercial/comparison_turbofan.html
-->

<turbine_engine name="CF6-80C2A3">
  <milthrust> 60200.0 </milthrust>
  <bypassratio>     5.31 </bypassratio>
  <tsfc>            0.576 </tsfc>
  <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   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">atmosphere/density-altitude</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   0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0000  0.0
    </tableData>
   </table>
  </function>

</turbine_engine>