<?xml version="1.0"?>
<!--
  File:     F119-PW-100.xml
  Author:   Aero-Matic v 0.8

  Inputs:
    name:           F119-PW-100
    type:           turbine
    thrust:         37000.8 lb
    augmented?      yes
    injected?       no
-->

<turbine_engine name="F119-PW-100">
  <milthrust>   26950.0 </milthrust>
  <maxthrust>   37000.0 </maxthrust>
  <bypassratio>     0.2 </bypassratio>
  <tsfc>            0.8 </tsfc>
  <atsfc>           1.95 </atsfc>
  <idlen1>         40.0 </idlen1>
  <idlen2>         53.0 </idlen2>
  <maxn1>         100.0 </maxn1>
  <maxn2>         100.0 </maxn2>
  <augmented>         1 </augmented>
  <augmethod>         1 </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   70000  80000
     0.0   1.2600  1.0000  0.7400  0.5340  0.3720  0.2410  0.1490  0.0800  0.040  0.0
     0.2   1.1710  0.9340  0.6970  0.5060  0.3550  0.2310  0.1430  0.0780  0.040  0.0
     0.4   1.1500  0.9210  0.6920  0.5060  0.3570  0.2330  0.1450  0.0790  0.040  0.0
     0.6   1.1810  0.9510  0.7210  0.5320  0.3780  0.2480  0.1540  0.0850  0.045  0.0
     0.8   1.2580  1.0200  0.7820  0.5820  0.4170  0.2750  0.1700  0.0935  0.045  0.0
     1.0   1.3690  1.1760  0.9135  0.6836  0.4988  0.3308  0.2048  0.1127  0.052  0.0
     1.2   1.4850  1.2915  1.0238  0.7812  0.5723  0.3780  0.2363  0.1300  0.065  0.0
     1.4   1.5941  1.4070  1.1403  0.8873  0.6595  0.4452  0.2762  0.1520  0.076  0.0
     1.6   1.6211  1.5250  1.2450  0.9890  0.7774  0.5260  0.3211  0.1767  0.087  0.0
     1.8   1.6211  1.6290  1.3474  1.0950  0.8774  0.6160  0.3811  0.2096  0.104  0.0
     2.0   1.6211  1.6000  1.4300  1.1850  0.9500  0.7050  0.4435  0.2420  0.121  0.0
     2.2   1.6211  1.6000  1.3600  1.1000  0.8600  0.6167  0.4000  0.2050  0.100  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   70000  80000
     0.0    1.1816  1.0000  0.8184  0.6627  0.5280  0.3756  0.2327  0.1279  0.063  0.0
     0.2    1.1308  0.9599  0.7890  0.6406  0.5116  0.3645  0.2258  0.1242  0.062  0.0
     0.4    1.1150  0.9474  0.7798  0.6340  0.5070  0.3615  0.2240  0.1232  0.061  0.0
     0.6    1.1284  0.9589  0.7894  0.6420  0.5134  0.3661  0.2268  0.1240  0.062  0.0
     0.8    1.1707  0.9990  0.8177  0.6647  0.5309  0.3784  0.2345  0.1290  0.065  0.0
     1.0    1.2411  1.1056  0.9080  0.7367  0.5876  0.4182  0.2590  0.1425  0.071  0.0
     1.2    1.3287  1.1817  0.9682  0.7835  0.6233  0.4430  0.2745  0.1513  0.075  0.0
     1.4    1.4365  1.2756  1.0430  0.8422  0.6678  0.4735  0.2933  0.1613  0.081  0.0
     1.6    1.5711  1.3923  1.1349  0.9135  0.7218  0.5103  0.3162  0.1739  0.085  0.0
     1.8    1.7301  1.5307  1.2449  0.9987  0.7870  0.5553  0.3441  0.1893  0.095  0.0
     2.0    1.8314  1.6485  1.3740  1.1000  0.8627  0.6708  0.3764  0.2070  0.103  0.0
     2.2    1.9700  1.7745  1.4805  1.3020  0.9555  0.6676  0.4137  0.2275  0.115  0.0	
     2.4    2.0700  1.8900  1.6065  1.4070  1.0500  0.7560  0.4830  0.2657  0.138  0.0
     2.6    2.2000  2.0160  1.7220  1.5120  1.1550  0.8400  0.5460  0.3003  0.150  0.0

	</tableData>
   </table>
  </function>

</turbine_engine>
