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A320-family/Engines/v2527_a5_2.xml

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<?xml version="1.0"?>
<!-- Copyright (c) 2020 Josh Davidson (Octal450) -->
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<turbine_engine name="V2527_A5">
<!-- data measured from https://www.youtube.com/watch?v=gPRQcYNRV_U -->
<milthrust> 24800 </milthrust>
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<tsfc> 0.445 </tsfc>
<bleed> 0.03 </bleed>
<ignitionn1> 4.8 </ignitionn1>
<ignitionn2> 23.9</ignitionn2>
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<idlen1> 22.4 </idlen1>
<idlen2> 60.9 </idlen2>
<n1spinup> 0.2 </n1spinup>
<n2spinup> 1.0 </n2spinup>
<n1startrate> 0.365 </n1startrate>
<n2startrate> 0.724 </n2startrate>
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<maxn1> 103.8 </maxn1>
<maxn2> 101.4 </maxn2>
<augmented> 0 </augmented>
<injected> 0 </injected>
<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>
<function name="N2SpoolUp">
<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="N2SpoolDown">
<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="IdleThrust">
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<independentVar lookup="column">atmosphere/density-altitude</independentVar>
<tableData>
-10000 0 10000 20000 30000 40000 50000
0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
</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
0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
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>
</function>
</turbine_engine>