Engine: Fix fuel consumption model, improve behavior of IAE thrust bump
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41eace24fb
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10 changed files with 12 additions and 12 deletions
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@ -53,11 +53,11 @@
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</text>
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<text>
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<halign>center</halign>
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<label>This is a complex simulation of these amazing Airbus Aircraft.</label>
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<label>This is a complex simulation of these amazing Airbus aircraft.</label>
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</text>
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<text>
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<halign>center</halign>
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<label>Use the Aircraft Config to select livery, manage panel states, and more!</label>
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<label>Use Aircraft Config to select livery, manage panel states, and more!</label>
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</text>
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</group>
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<turbine_engine name="CFM56-5B4">
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<milthrust>27000</milthrust>
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<tsfc>0.445</tsfc>
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<tsfc>0.335</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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@ -5,7 +5,7 @@
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<turbine_engine name="CFM56-5B4">
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<milthrust>27000</milthrust>
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<tsfc>0.445</tsfc>
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<tsfc>0.335</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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@ -5,7 +5,7 @@
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<turbine_engine name="LEAP-1A26">
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<milthrust>27000</milthrust>
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<tsfc>0.445</tsfc>
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<tsfc>0.335</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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@ -5,7 +5,7 @@
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<turbine_engine name="LEAP-1A26">
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<milthrust>27000</milthrust>
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<tsfc>0.445</tsfc>
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<tsfc>0.335</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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@ -5,7 +5,7 @@
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<turbine_engine name="PW1127G-JM">
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<milthrust>27000</milthrust>
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<tsfc>0.445</tsfc>
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<tsfc>0.335</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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@ -5,7 +5,7 @@
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<turbine_engine name="PW1127G-JM">
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<milthrust>27000</milthrust>
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<tsfc>0.445</tsfc>
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<tsfc>0.335</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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@ -5,7 +5,7 @@
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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>0.445</tsfc>
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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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@ -5,7 +5,7 @@
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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>0.445</tsfc>
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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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@ -39,8 +39,8 @@
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<tableData>
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0.080 0.973269699530
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0.090 1.000000000000
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0.06 0.973269699530
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0.10 1.000000000000
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</tableData>
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</table>
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</function>
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