128 lines
3.6 KiB
XML
128 lines
3.6 KiB
XML
<?xml version="1.0"?>
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<!-- Copyright (c) 2021 Josh Davidson (Octal450) -->
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<turbine_engine name="V2527-A5">
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<milthrust>26600</milthrust> <!-- @ 0.2 Mach, 24800 at 0 Mach, handled in fadec file -->
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<tsfc>0.335</tsfc>
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<bleed>0.03</bleed>
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<ignitionn1>4.8</ignitionn1>
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<ignitionn2>23.9</ignitionn2>
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<n1spinup>0.37</n1spinup>
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<n2spinup>1.85</n2spinup>
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<n1startrate>0.365</n1startrate>
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<n2startrate>0.767</n2startrate>
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<idlen1>22.4</idlen1>
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<idlen2>60.9</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="N1SpoolUp">
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<table>
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<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
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<tableData>
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24 1.1
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28 2.9
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46 9.7
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68 15.4
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80 19.6
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94 21.4
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103 23.6
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</tableData>
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</table>
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</function>
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<function name="N1SpoolDown">
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<table>
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<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
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<tableData>
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24 1.1
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28 2.9
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46 9.7
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68 15.4
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80 19.6
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94 21.4
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103 23.6
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</tableData>
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</table>
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</function>
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<function name="N2SpoolUp"> <!-- N1 to N2 factor 0.503865979381443 -->
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<table>
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<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
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<tableData>
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24 0.6
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28 1.5
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46 4.9
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68 7.8
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80 9.9
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94 10.8
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103 11.9
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</tableData>
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</table>
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</function>
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<function name="N2SpoolDown"> <!-- N1 to N2 factor 0.503865979381443 -->
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<table>
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<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
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<tableData>
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24 0.6
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28 1.5
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46 4.9
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68 7.8
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80 9.9
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94 10.8
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103 11.9
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</tableData>
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</table>
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</function>
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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 43000 50000
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0.0 0.0430 0.0458 0.0378 0.0684 0.0654 0.0623 0.0000
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0.2 0.0500 0.0291 0.0205 0.0514 0.0539 0.0563 0.0000
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0.4 0.0040 0.0047 0.0012 0.0412 0.0460 0.0507 0.0000
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0.6 0.0000 0.0000 0.0000 0.0000 0.0181 0.0362 0.0000
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0.8 0.0000 0.0000 0.0000 0.0000 0.0158 0.0315 0.0000
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1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0204 0.0000
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1.2 0.0000 0.0000 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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<function name="MilThrust"> <!-- If you change this, make sure you update the table in the engine system file -->
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<product>
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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 43000 50000
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0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2840 0.0000
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0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2740 0.0000
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0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2670 0.0000
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0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2310 0.0000
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0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.2060 0.0000
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0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1270 0.0000
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1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0580 0.0000
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1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
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</tableData>
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</table>
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<property>fadec/limit/rated-thrust-factor</property>
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<table> <!-- Thrust loss due to reverser angle -->
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<independentVar lookup="row">/engines/engine[1]/reverser-pos-norm</independentVar>
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<tableData>
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0.01 1.00
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1.00 0.65
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</tableData>
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</table>
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</product>
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</function>
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</turbine_engine>
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