118 lines
3.2 KiB
XML
118 lines
3.2 KiB
XML
<?xml version="1.0"?>
|
|
|
|
<!-- Copyright (c) 2019 Joshua Davidson (Octal450) -->
|
|
|
|
<turbine_engine name="LEAP1A26">
|
|
|
|
<milthrust> 27000 </milthrust>
|
|
<tsfc> 0.445 </tsfc>
|
|
<bleed> 0.03 </bleed>
|
|
<ignitionn1> 0.6 </ignitionn1>
|
|
<ignitionn2> 22.2</ignitionn2>
|
|
<idlen1> 18.9 </idlen1>
|
|
<idlen2> 59.4 </idlen2>
|
|
<n1spinup> 0.05 </n1spinup>
|
|
<n2spinup> 1.85 </n2spinup>
|
|
<n1startrate> 0.573 </n1startrate>
|
|
<n2startrate> 1.127 </n2startrate>
|
|
<maxn1> 103.8 </maxn1>
|
|
<maxn2> 101.4 </maxn2>
|
|
<augmented> 0 </augmented>
|
|
<injected> 0 </injected>
|
|
|
|
<function name="N1SpoolUp">
|
|
<table>
|
|
<independentVar lookup="row">/engines/engine[0]/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[0]/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[0]/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[0]/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>
|