62 lines
2.2 KiB
XML
62 lines
2.2 KiB
XML
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<?xml version="1.0"?>
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<!--
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File: trent_xwb.xml
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Author: Aero-Matic v 0.82
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Inputs:
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name: trent_xwb
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type: turbine
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thrust: 97000 lb
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augmented? no
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injected? no
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-->
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<turbine_engine name="trent_xwb">
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<milthrust> 84000.0 </milthrust>
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<bypassratio> 1.0 </bypassratio>
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<tsfc> 0.48 </tsfc>
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<bleed> 0.03</bleed>
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<idlen1> 20.0 </idlen1>
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<idlen2> 60.0 </idlen2>
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<maxn1> 100.0 </maxn1>
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<maxn2> 100.0 </maxn2>
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<augmented> 0 </augmented>
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<injected> 0 </injected>
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<function name="IdleThrust">
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<independentVar lookup="column">atmosphere/density-altitude</independentVar>
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<tableData>
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-10000 0 10000 20000 30000 40000 50000 60000
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0.0 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467 0
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0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342 0
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0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203 0
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0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073 0
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0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900 0
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1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800 0
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</tableData>
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</table>
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</function>
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<function name="MilThrust">
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<independentVar lookup="column">atmosphere/density-altitude</independentVar>
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<tableData>
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-10000 0 10000 20000 30000 40000 50000 60000
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0.0 1.2600 1.0000 0.7400 0.5340 0.3720 0.2810 0.1490 0
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0.2 1.1710 0.9340 0.6970 0.5060 0.3550 0.2810 0.1430 0
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0.4 1.1500 0.9210 0.6920 0.5060 0.3570 0.2830 0.1450 0
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0.6 1.1810 0.9510 0.7210 0.5320 0.3780 0.2880 0.1540 0
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0.8 1.2580 1.0200 0.7820 0.5820 0.4170 0.3150 0.1700 0
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1.0 1.3690 1.1200 0.8710 0.6510 0.4750 0.3550 0.1950 0
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1.2 1.4850 1.2300 0.9750 0.7440 0.5450 0.4040 0.2250 0
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1.4 1.5941 1.3400 1.0860 0.8450 0.6280 0.4640 0.2630 0
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</tableData>
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</table>
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</function>
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</turbine_engine>
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