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A320-family/Engines/v2527-a5_2.xml

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<?xml version="1.0"?>
<!-- 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 -->
<tsfc>0.335</tsfc>
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<bleed>0.03</bleed>
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<ignitionn1>4.8</ignitionn1>
<ignitionn2>23.9</ignitionn2>
<n1spinup>0.2</n1spinup>
<n2spinup>1.0</n2spinup>
<n1startrate>0.365</n1startrate>
<n2startrate>1.724</n2startrate>
<idlen1>22.4</idlen1>
<idlen2>60.9</idlen2>
<maxn1>100.0</maxn1>
<maxn2>100.0</maxn2>
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<augmented>0</augmented>
<injected>0</injected>
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<function name="N1SpoolUp">
<table>
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
<tableData>
24 1.1
28 2.9
46 9.7
68 15.4
80 19.6
94 21.4
103 23.6
</tableData>
</table>
</function>
<function name="N1SpoolDown">
<table>
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
<tableData>
24 1.1
28 2.9
46 9.7
68 15.4
80 19.6
94 21.4
103 23.6
</tableData>
</table>
</function>
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<function name="N2SpoolUp"> <!-- N1 to N2 factor 0.503865979381443 -->
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<table>
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
<tableData>
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24 0.6
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28 1.5
46 4.9
68 7.8
80 9.9
94 10.8
103 11.9
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</tableData>
</table>
</function>
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<function name="N2SpoolDown"> <!-- N1 to N2 factor 0.503865979381443 -->
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<table>
<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
<tableData>
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24 0.6
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28 1.5
46 4.9
68 7.8
80 9.9
94 10.8
103 11.9
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</tableData>
</table>
</function>
<function name="IdleThrust">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
<tableData>
-10000 0 10000 20000 30000 43000 50000
0.0 0.0430 0.0458 0.0378 0.0684 0.0654 0.0623 0.0000
0.2 0.0500 0.0291 0.0205 0.0514 0.0539 0.0563 0.0000
0.4 0.0040 0.0047 0.0012 0.0412 0.0460 0.0507 0.0000
0.6 0.0000 0.0000 0.0000 0.0000 0.0181 0.0362 0.0000
0.8 0.0000 0.0000 0.0000 0.0000 0.0158 0.0315 0.0000
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0204 0.0000
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</tableData>
</table>
</function>
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<function name="MilThrust"> <!-- If you change this, make sure you update the table in the engine system file -->
<product>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
<tableData>
-10000 0 10000 20000 30000 43000 50000
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2840 0.0000
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2740 0.0000
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2670 0.0000
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2310 0.0000
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.2060 0.0000
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1270 0.0000
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
1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
</tableData>
</table>
<property>fadec/limit/rated-thrust-factor</property>
<table> <!-- Thrust loss due to reverser angle -->
<independentVar lookup="row">/engines/engine[1]/reverser-pos-norm</independentVar>
<tableData>
0.01 1.00
1.00 0.65
</tableData>
</table>
</product>
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</function>
</turbine_engine>