52 lines
2.1 KiB
XML
52 lines
2.1 KiB
XML
<?xml version="1.0"?>
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<turbine_engine name="V2527_A5">
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<milthrust> 26600 </milthrust> <!-- Will put proper thrust amount once FDE sorted out -->
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<bypassratio> 7.1 </bypassratio>
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<tsfc> 0.8 </tsfc>
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<bleed> 0.03 </bleed>
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<idlen1> 22.4 </idlen1>
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<idlen2> 60.9 </idlen2>
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<n1spinup> 0.2 </n1spinup>
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<n2spinup> 2.0 </n2spinup>
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<maxn1> 105.8 </maxn1>
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<maxn2> 102.1 </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
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0.0 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
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0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
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0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
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0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073
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0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900
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1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800
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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
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0.0 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490
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0.2 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
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0.4 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
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0.6 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
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0.8 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1600
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0.9 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.0000
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1.0 1.1810 0.9510 0.7210 0.5320 0.3780 0.0000 0.0000
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1.2 1.1500 0.9210 0.6920 0.0000 0.0000 0.0000 0.0000
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1.4 1.1710 0.9340 0.0000 0.0000 0.0000 0.0000 0.0000
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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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