[Flightgear-cvslogs] CVS: data/Aircraft/L-1011-500/Engines RB211-524B.xml, NONE, 1.1 direct.xml, NONE, 1.1

[Emmanuel B. <he...@ba...>]

Update of /var/cvs/FlightGear-0.9/data/Aircraft/L-1011-500/Engines
In directory baron.flightgear.org:/tmp/cvs-serv22228/Engines

Added Files:
	RB211-524B.xml direct.xml 
Log Message:
- New plane

--- NEW FILE "RB211-524B.xml" ---
<?xml version="1.0"?>
<!--
  File:     RB211-524B.xml
  Author:   Aero-Matic v 0.81

  Inputs:
    name:           RB211-524B
    type:           turbine
    thrust:         50000 lb
    augmented?      no
    injected?       no
-->

<turbine_engine name="RB211-524B">
  <milthrust> 50000.0 </milthrust>
  <bypassratio>     4.50 </bypassratio>
  <tsfc>            0.65 </tsfc>
  <bleed>           0.03</bleed>
  <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
     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>

</turbine_engine>

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