CVS: data/Aircraft/Lockheed-NF104/Engines J79-GE-11A.xml, NONE, 1.1 direct.xml, NONE, 1.1

Update of /var/cvs/FlightGear-0.9/data/Aircraft/Lockheed-NF104/Engines
In directory baron.flightgear.org:/tmp/cvs-serv23742/Engines

Added Files:
	J79-GE-11A.xml direct.xml 
Log Message:
- New NF 104 C (by separate NF 104 A and NF 104 C)

--- NEW FILE "J79-GE-11A.xml" ---
<?xml version="1.0"?>
<!--
  File:     J79-GE-11A.xml
  Author:   Aero-Matic v 0.8

  Inputs:
    name:           J79-GE-11A
    type:           turbine
    thrust:         10000.0 lb
    augmented?      yes
    injected?       no
-->

<turbine_engine name="J79">
  <milthrust>   10000.0 </milthrust>
  <maxthrust>   15800.0 </maxthrust>
  <bypassratio>     0.0 </bypassratio>
  <tsfc>            0.95 </tsfc>
  <atsfc>           1.90 </atsfc>
  <bleed>           0.03 </bleed>
  <idlen1>         33.5 </idlen1>
  <idlen2>         67.0 </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
     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>

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

</turbine_engine>

--- NEW FILE "direct.xml" ---
<?xml version="1.0"?>
<!--
  Thrust is computed directly by the engine
-->
<direct name="Direct">
</direct>


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