A350-family/Engines/trent_xwb.xml

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<?xml version="1.0"?>
<!--
File: trent_xwb.xml
Author: Aero-Matic v 0.82
Inputs:
name: trent_xwb
type: turbine
thrust: 97000 lb
augmented? no
injected? no
-->
<turbine_engine name="trent_xwb">
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<milthrust> 84200.0 </milthrust>
<bypassratio> 1.0 </bypassratio>
<tsfc> 0.48 </tsfc>
<bleed> 0.03</bleed>
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<idlen1> 21.4 </idlen1>
<idlen2> 60.0 </idlen2>
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<maxn1> 99.1 </maxn1>
<maxn2> 100.2 </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 60000
0.0 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467 0
0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342 0
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203 0
0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073 0
0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900 0
1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800 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 0.2810 0.1490 0
0.2 1.1710 0.9340 0.6970 0.5060 0.3550 0.2810 0.1430 0
0.4 1.1500 0.9210 0.6920 0.5060 0.3570 0.2830 0.1450 0
0.6 1.1810 0.9510 0.7210 0.5320 0.3780 0.2880 0.1540 0
0.8 1.2580 1.0200 0.7820 0.5820 0.4170 0.3150 0.1700 0
1.0 1.3690 1.1200 0.8710 0.6510 0.4750 0.3550 0.1950 0
1.2 1.4850 1.2300 0.9750 0.7440 0.5450 0.4040 0.2250 0
1.4 1.5941 1.3400 1.0860 0.8450 0.6280 0.4640 0.2630 0
</tableData>
</table>
</function>
</turbine_engine>