We don't need you
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legoboyvdlp R
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2 changed files with 0 additions and 238 deletions
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<?xml version="1.0"?>
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<!-- Copyright (c) 2020 Josh Davidson (Octal450) -->
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<turbine_engine name="CFM56_5A1">
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<!-- source https://www.youtube.com/watch?v=jnGfzv7Odh4 -->
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<milthrust> 25000 </milthrust>
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<tsfc> 0.445 </tsfc>
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<bleed> 0.03 </bleed>
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<ignitionn1> 0.6 </ignitionn1>
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<ignitionn2> 22.2</ignitionn2>
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<idlen1> 18.9 </idlen1>
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<idlen2> 59.4 </idlen2>
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<n1spinup> 0.05 </n1spinup>
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<n2spinup> 1.85 </n2spinup>
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<n1startrate> 0.573 </n1startrate>
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<n2startrate> 1.127 </n2startrate>
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<maxn1> 103.8 </maxn1>
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<maxn2> 101.4 </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[0]/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[0]/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">
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<table>
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<independentVar lookup="row">/engines/engine[0]/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="N2SpoolDown">
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<table>
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<independentVar lookup="row">/engines/engine[0]/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="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 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
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0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
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0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
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0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
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0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
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1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
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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 0.5640 0.3920 0.2710 0.0000
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0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
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0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
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0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
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0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
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0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
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1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 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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1.4 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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</turbine_engine>
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@ -1,119 +0,0 @@
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<?xml version="1.0"?>
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<!-- Copyright (c) 2020 Josh Davidson (Octal450) -->
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<turbine_engine name="CFM56_5A1">
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<!-- source https://www.youtube.com/watch?v=jnGfzv7Odh4 -->
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<milthrust> 25000 </milthrust>
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<tsfc> 0.445 </tsfc>
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<bleed> 0.03 </bleed>
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<ignitionn1> 0.6 </ignitionn1>
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<ignitionn2> 22.2</ignitionn2>
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<idlen1> 18.9 </idlen1>
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<idlen2> 59.4 </idlen2>
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<n1spinup> 0.05 </n1spinup>
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<n2spinup> 1.85 </n2spinup>
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<n1startrate> 0.573 </n1startrate>
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<n2startrate> 1.127 </n2startrate>
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<maxn1> 103.8 </maxn1>
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<maxn2> 101.4 </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">
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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="N2SpoolDown">
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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="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 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
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0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
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0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
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0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
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0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
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1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
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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 0.5640 0.3920 0.2710 0.0000
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0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
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0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
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0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
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0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
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0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
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1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 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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1.4 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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</turbine_engine>
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