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Engine: Fix fuel consumption model, improve behavior of IAE thrust bump

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This commit is contained in:
Josh Davidson 2021-10-10 12:04:00 -04:00
parent 41eace24fb
commit 68533de7f6
10 changed files with 12 additions and 12 deletions
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4
AircraftConfig/welcome.xml
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@ -53,11 +53,11 @@
</text> </text>
<text> <text>
<halign>center</halign> <halign>center</halign>
<label>This is a complex simulation of these amazing Airbus Aircraft.</label> <label>This is a complex simulation of these amazing Airbus aircraft.</label>
</text> </text>
<text> <text>
<halign>center</halign> <halign>center</halign>
<label>Use the Aircraft Config to select livery, manage panel states, and more!</label> <label>Use Aircraft Config to select livery, manage panel states, and more!</label>
</text> </text>
</group> </group>

2
Engines/cfm56-5b4_1.xml
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@ -5,7 +5,7 @@
<turbine_engine name="CFM56-5B4"> <turbine_engine name="CFM56-5B4">
<milthrust>27000</milthrust> <milthrust>27000</milthrust>
<tsfc>0.445</tsfc> <tsfc>0.335</tsfc>
<bleed>0.03</bleed> <bleed>0.03</bleed>
<ignitionn1>0.6</ignitionn1> <ignitionn1>0.6</ignitionn1>
<ignitionn2>22.2</ignitionn2> <ignitionn2>22.2</ignitionn2>

2
Engines/cfm56-5b4_2.xml
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@ -5,7 +5,7 @@
<turbine_engine name="CFM56-5B4"> <turbine_engine name="CFM56-5B4">
<milthrust>27000</milthrust> <milthrust>27000</milthrust>
<tsfc>0.445</tsfc> <tsfc>0.335</tsfc>
<bleed>0.03</bleed> <bleed>0.03</bleed>
<ignitionn1>0.6</ignitionn1> <ignitionn1>0.6</ignitionn1>
<ignitionn2>22.2</ignitionn2> <ignitionn2>22.2</ignitionn2>

2
Engines/leap1a26_1.xml
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@ -5,7 +5,7 @@
<turbine_engine name="LEAP-1A26"> <turbine_engine name="LEAP-1A26">
<milthrust>27000</milthrust> <milthrust>27000</milthrust>
<tsfc>0.445</tsfc> <tsfc>0.335</tsfc>
<bleed>0.03</bleed> <bleed>0.03</bleed>
<ignitionn1>0.6</ignitionn1> <ignitionn1>0.6</ignitionn1>
<ignitionn2>22.2</ignitionn2> <ignitionn2>22.2</ignitionn2>

2
Engines/leap1a26_2.xml
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@ -5,7 +5,7 @@
<turbine_engine name="LEAP-1A26"> <turbine_engine name="LEAP-1A26">
<milthrust>27000</milthrust> <milthrust>27000</milthrust>
<tsfc>0.445</tsfc> <tsfc>0.335</tsfc>
<bleed>0.03</bleed> <bleed>0.03</bleed>
<ignitionn1>0.6</ignitionn1> <ignitionn1>0.6</ignitionn1>
<ignitionn2>22.2</ignitionn2> <ignitionn2>22.2</ignitionn2>

2
Engines/pw1127g_1.xml
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@ -5,7 +5,7 @@
<turbine_engine name="PW1127G-JM"> <turbine_engine name="PW1127G-JM">
<milthrust>27000</milthrust> <milthrust>27000</milthrust>
<tsfc>0.445</tsfc> <tsfc>0.335</tsfc>
<bleed>0.03</bleed> <bleed>0.03</bleed>
<ignitionn1>0.6</ignitionn1> <ignitionn1>0.6</ignitionn1>
<ignitionn2>22.2</ignitionn2> <ignitionn2>22.2</ignitionn2>

2
Engines/pw1127g_2.xml
View file

@ -5,7 +5,7 @@
<turbine_engine name="PW1127G-JM"> <turbine_engine name="PW1127G-JM">
<milthrust>27000</milthrust> <milthrust>27000</milthrust>
<tsfc>0.445</tsfc> <tsfc>0.335</tsfc>
<bleed>0.03</bleed> <bleed>0.03</bleed>
<ignitionn1>0.6</ignitionn1> <ignitionn1>0.6</ignitionn1>
<ignitionn2>22.2</ignitionn2> <ignitionn2>22.2</ignitionn2>

2
Engines/v2527-a5_1.xml
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@ -5,7 +5,7 @@
<turbine_engine name="V2527-A5"> <turbine_engine name="V2527-A5">
<milthrust>26600</milthrust> <!-- @ 0.2 Mach, 24800 at 0 Mach, handled in fadec file --> <milthrust>26600</milthrust> <!-- @ 0.2 Mach, 24800 at 0 Mach, handled in fadec file -->
<tsfc>0.445</tsfc> <tsfc>0.335</tsfc>
<bleed>0.03</bleed> <bleed>0.03</bleed>
<ignitionn1>4.8</ignitionn1> <ignitionn1>4.8</ignitionn1>
<ignitionn2>23.9</ignitionn2> <ignitionn2>23.9</ignitionn2>

2
Engines/v2527-a5_2.xml
View file

@ -5,7 +5,7 @@
<turbine_engine name="V2527-A5"> <turbine_engine name="V2527-A5">
<milthrust>26600</milthrust> <!-- @ 0.2 Mach, 24800 at 0 Mach, handled in fadec file --> <milthrust>26600</milthrust> <!-- @ 0.2 Mach, 24800 at 0 Mach, handled in fadec file -->
<tsfc>0.445</tsfc> <tsfc>0.335</tsfc>
<bleed>0.03</bleed> <bleed>0.03</bleed>
<ignitionn1>4.8</ignitionn1> <ignitionn1>4.8</ignitionn1>
<ignitionn2>23.9</ignitionn2> <ignitionn2>23.9</ignitionn2>

4
Systems/a320-v2527-a5-engine-fadec.xml
View file

@ -39,8 +39,8 @@
<table> <table>
<independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="row">velocities/mach</independentVar>
<tableData> <tableData>
0.080 0.973269699530 0.06 0.973269699530
0.090 1.000000000000 0.10 1.000000000000
</tableData> </tableData>
</table> </table>
</function> </function>