jsbsim.js/JSBSim/engine/GE-CF6-80C2-B1F.xml

JSBSim flight dynamics model ported to JavaScript

<?xml version="1.0"?>
<!--
  File:     GE-CF6-80C2-B1F.xml
  Author:   Jon Berndt, Aero-Matic v 0.8

  Inputs:
    name:           GE-CF6-80C2-B1F
    type:           turbine
    thrust:         58000.0 lb
    augmented?      no
    injected?       yes

  Additional Information:

  [Source: http://www.bh.com/companions/034074152X/appendices/data-b/table-3/default.htm]

    Number of shafts: 2
    Compressor: 1 + 4LP
                14HP
    Turbine:    2HP, 5LP
    Cost: $6.10 million

    Length: 14.00 ft.
    Fan diameter: 8.84 ft.
    Weight: 9,500 lbs.

    Flat rating: 32 degrees C
    Pressure ratio (TO): 29.90
    Mass flow (lb/sec, TO): 1,765 (lb/sec)
    TSFC (TO): 0.32
-->

<turbine_engine name="GE-CF6-80C2-B1F">
  <milthrust>   58000.0 </milthrust>
  <bypassratio>     5.15 </bypassratio>
  <tsfc>            0.564 </tsfc>
  <idlen1>         30.0 </idlen1>
  <idlen2>         60.0 </idlen2>
  <maxn1>         100.0 </maxn1>
  <maxn2>         100.0 </maxn2>
  <augmented>         0 </augmented>
  <augmethod>         1 </augmethod>
  <injected>          1 </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   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>