<?xml version="1.0"?>
<!--
  File:     F100-PW-229.xml
  Author:   Aero-Matic v 0.8

  Inputs:
    name:           F100
    type:           turbine
    thrust:         17800 lb
    augmented?      yes
    injected?       no
-->

<turbine_engine name="F100">
  <milthrust>   17800.0 </milthrust>
  <maxthrust>   29000.0 </maxthrust>
  <bypassratio>     0.4 </bypassratio>
  <tsfc>            0.74 </tsfc>
  <atsfc>           2.05 </atsfc>
  <idlen1>         40.0 </idlen1>
  <idlen2>         53.0 </idlen2>
  <maxn1>         100.0 </maxn1>
  <maxn2>         100.0 </maxn2>
  <augmented>         1 </augmented>
  <augmethod>         2 </augmethod>
  <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   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>

  <function name="AugThrust">
   <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    1.1816  1.0000  0.8184  0.6627  0.5280  0.3756  0.2327  0.0
     0.2    1.1308  0.9599  0.7890  0.6406  0.5116  0.3645  0.2258  0.0
     0.4    1.1150  0.9474  0.7798  0.6340  0.5070  0.3615  0.2240  0.0
     0.6    1.1284  0.9589  0.7894  0.6420  0.5134  0.3661  0.2268  0.0
     0.8    1.1707  0.9942  0.8177  0.6647  0.5309  0.3784  0.2345  0.0
     1.0    1.2411  1.0529  0.8648  0.7017  0.5596  0.3983  0.2467  0.0
     1.2    1.3287  1.1254  0.9221  0.7462  0.5936  0.4219  0.2614  0.0
     1.4    1.4365  1.2149  0.9933  0.8021  0.6360  0.4509  0.2794  0.0
     1.6    1.5711  1.3260  1.0809  0.8700  0.6874  0.4860  0.3011  0.0
     1.8    1.7301  1.4579  1.1857  0.9512  0.7495  0.5289  0.3277  0.0
     2.0    1.8314  1.5700  1.3086  1.0474  0.8216  0.5786  0.3585  0.0
     2.2    1.9700  1.6900  1.4100  1.2400  0.9100  0.6359  0.3940  0.0
     2.4    2.0700  1.8000  1.5300  1.3400  1.0000  0.7200  0.4600  0.0
     2.6    2.2000  1.9200  1.6400  1.4400  1.1000  0.8000  0.5200  0.0
    </tableData>
   </table>
  </function>

</turbine_engine>
