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A32X: Cleanup

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This commit is contained in:
Joshua Davidson 2017-10-20 14:05:58 -04:00
parent c122b65292
commit 3b71d1337e
17 changed files with 17 additions and 489 deletions
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4
A318-100-CFM.xml
View file

@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</ground_reactions>
<propulsion>
<engine file="cfm56_5b9">
<engine file="cfm56_5b4">
<location unit="M">
<x> 14.3962788 </x>
<y> -5.755 </y>
@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</thruster>
</engine>
<engine file="cfm56_5b9">
<engine file="cfm56_5b4">
<location unit="M">
<x> 14.3962788 </x>
<y> 5.755 </y>

4
A319-100-CFM.xml
View file

@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</ground_reactions>
<propulsion>
<engine file="cfm56_5b6">
<engine file="cfm56_5b4">
<location unit="M">
<x> 14.3962788 </x>
<y> -5.755 </y>
@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</thruster>
</engine>
<engine file="cfm56_5b6">
<engine file="cfm56_5b4">
<location unit="M">
<x> 14.3962788 </x>
<y> 5.755 </y>

4
A319-100-IAE.xml
View file

@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</ground_reactions>
<propulsion>
<engine file="v2522_a5">
<engine file="v2527_a5">
<location unit="M">
<x> 14.3962788 </x>
<y> -5.755 </y>
@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</thruster>
</engine>
<engine file="v2522_a5">
<engine file="v2527_a5">
<location unit="M">
<x> 14.3962788 </x>
<y> 5.755 </y>

4
A320-100-CFM.xml
View file

@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</ground_reactions>
<propulsion>
<engine file="cfm56_5a1">
<engine file="cfm56_5a4">
<location unit="M">
<x> 14.3962788 </x>
<y> -5.755 </y>
@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</thruster>
</engine>
<engine file="cfm56_5a1">
<engine file="cfm56_5a4">
<location unit="M">
<x> 14.3962788 </x>
<y> 5.755 </y>

4
A321-200-CFM.xml
View file

@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</ground_reactions>
<propulsion>
<engine file="cfm56_5b3">
<engine file="cfm56_5b4">
<location unit="M">
<x> 14.3962788 </x>
<y> -5.755 </y>
@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</thruster>
</engine>
<engine file="cfm56_5b3">
<engine file="cfm56_5b4">
<location unit="M">
<x> 14.3962788 </x>
<y> 5.755 </y>

4
A321-200-IAE.xml
View file

@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</ground_reactions>
<propulsion>
<engine file="v2533_a5">
<engine file="v2527_a5">
<location unit="M">
<x> 14.3962788 </x>
<y> -5.755 </y>
@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</thruster>
</engine>
<engine file="v2533_a5">
<engine file="v2527_a5">
<location unit="M">
<x> 14.3962788 </x>
<y> 5.755 </y>

4
A321neo-CFM.xml
View file

@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</ground_reactions>
<propulsion>
<engine file="leap1a32">
<engine file="leap1a26">
<location unit="M">
<x> 14.3962788 </x>
<y> -5.755 </y>
@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</thruster>
</engine>
<engine file="leap1a32">
<engine file="leap1a26">
<location unit="M">
<x> 14.3962788 </x>
<y> 5.755 </y>

4
A321neo-PW.xml
View file

@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</ground_reactions>
<propulsion>
<engine file="pw1133g">
<engine file="pw1127g">
<location unit="M">
<x> 14.3962788 </x>
<y> -5.755 </y>
@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
</thruster>
</engine>
<engine file="pw1133g">
<engine file="pw1127g">
<location unit="M">
<x> 14.3962788 </x>
<y> 5.755 </y>

59
Engines/cfm56_5a1.xml
View file

@ -1,59 +0,0 @@
<?xml version="1.0"?>
<!--
#########################################
# Copyright (c) it0uchpods Design Group #
#########################################
-->
<turbine_engine name="CFM56_5A1">
<milthrust> 27000 </milthrust>
<bypassratio> 8.1 </bypassratio>
<tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed>
<idlen1> 19.7 </idlen1>
<idlen2> 61.2 </idlen2>
<n1spinup> 0.2 </n1spinup>
<n2spinup> 2.0 </n2spinup>
<maxn1> 103.8 </maxn1>
<maxn2> 99.6 </maxn2>
<augmented> 0 </augmented>
<injected> 0 </injected>
<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 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073
0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900
1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800
</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 0.5440 0.3720 0.2410 0.0000
0.2 1.1710 0.9740 0.6970 0.5160 0.3650 0.2310 0.0000
0.4 1.1500 0.9570 0.6920 0.5260 0.3670 0.2230 0.0000
0.6 1.1810 0.9410 0.7210 0.5460 0.3380 0.1880 0.0000
0.8 1.2290 1.0200 0.7820 0.5370 0.2840 0.1450 0.0000
0.9 1.2580 1.0200 0.7820 0.5020 0.2510 0.0650 0.0000
1.0 1.1810 0.9510 0.7210 0.4210 0.1540 0.0150 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>

59
Engines/cfm56_5b3.xml
View file

@ -1,59 +0,0 @@
<?xml version="1.0"?>
<!--
#########################################
# Copyright (c) it0uchpods Design Group #
#########################################
-->
<turbine_engine name="CFM56_5B3">
<milthrust> 27000 </milthrust>
<bypassratio> 8.1 </bypassratio>
<tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed>
<idlen1> 19.7 </idlen1>
<idlen2> 61.2 </idlen2>
<n1spinup> 0.2 </n1spinup>
<n2spinup> 2.0 </n2spinup>
<maxn1> 103.8 </maxn1>
<maxn2> 99.6 </maxn2>
<augmented> 0 </augmented>
<injected> 0 </injected>
<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 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073
0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900
1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800
</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 0.5440 0.3720 0.2410 0.0000
0.2 1.1710 0.9740 0.6970 0.5160 0.3650 0.2310 0.0000
0.4 1.1500 0.9570 0.6920 0.5260 0.3670 0.2230 0.0000
0.6 1.1810 0.9410 0.7210 0.5460 0.3380 0.1880 0.0000
0.8 1.2290 1.0200 0.7820 0.5370 0.2840 0.1450 0.0000
0.9 1.2580 1.0200 0.7820 0.5020 0.2510 0.0650 0.0000
1.0 1.1810 0.9510 0.7210 0.4210 0.1540 0.0150 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>

59
Engines/cfm56_5b6.xml
View file

@ -1,59 +0,0 @@
<?xml version="1.0"?>
<!--
#########################################
# Copyright (c) it0uchpods Design Group #
#########################################
-->
<turbine_engine name="CFM56_5B6">
<milthrust> 27000 </milthrust>
<bypassratio> 8.1 </bypassratio>
<tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed>
<idlen1> 19.7 </idlen1>
<idlen2> 61.2 </idlen2>
<n1spinup> 0.2 </n1spinup>
<n2spinup> 2.0 </n2spinup>
<maxn1> 103.8 </maxn1>
<maxn2> 99.6 </maxn2>
<augmented> 0 </augmented>
<injected> 0 </injected>
<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 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073
0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900
1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800
</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 0.5440 0.3720 0.2410 0.0000
0.2 1.1710 0.9740 0.6970 0.5160 0.3650 0.2310 0.0000
0.4 1.1500 0.9570 0.6920 0.5260 0.3670 0.2230 0.0000
0.6 1.1810 0.9410 0.7210 0.5460 0.3380 0.1880 0.0000
0.8 1.2290 1.0200 0.7820 0.5370 0.2840 0.1450 0.0000
0.9 1.2580 1.0200 0.7820 0.5020 0.2510 0.0650 0.0000
1.0 1.1810 0.9510 0.7210 0.4210 0.1540 0.0150 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>

59
Engines/cfm56_5b9.xml
View file

@ -1,59 +0,0 @@
<?xml version="1.0"?>
<!--
#########################################
# Copyright (c) it0uchpods Design Group #
#########################################
-->
<turbine_engine name="CFM56_5B9">
<milthrust> 27000 </milthrust>
<bypassratio> 8.1 </bypassratio>
<tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed>
<idlen1> 19.7 </idlen1>
<idlen2> 61.2 </idlen2>
<n1spinup> 0.2 </n1spinup>
<n2spinup> 2.0 </n2spinup>
<maxn1> 103.8 </maxn1>
<maxn2> 99.6 </maxn2>
<augmented> 0 </augmented>
<injected> 0 </injected>
<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 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073
0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900
1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800
</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 0.5440 0.3720 0.2410 0.0000
0.2 1.1710 0.9740 0.6970 0.5160 0.3650 0.2310 0.0000
0.4 1.1500 0.9570 0.6920 0.5260 0.3670 0.2230 0.0000
0.6 1.1810 0.9410 0.7210 0.5460 0.3380 0.1880 0.0000
0.8 1.2290 1.0200 0.7820 0.5370 0.2840 0.1450 0.0000
0.9 1.2580 1.0200 0.7820 0.5020 0.2510 0.0650 0.0000
1.0 1.1810 0.9510 0.7210 0.4210 0.1540 0.0150 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>

59
Engines/leap1a32.xml
View file

@ -1,59 +0,0 @@
<?xml version="1.0"?>
<!--
#########################################
# Copyright (c) it0uchpods Design Group #
#########################################
-->
<turbine_engine name="LEAP1A32">
<milthrust> 27000 </milthrust>
<bypassratio> 8.1 </bypassratio>
<tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed>
<idlen1> 19.7 </idlen1>
<idlen2> 61.2 </idlen2>
<n1spinup> 0.2 </n1spinup>
<n2spinup> 2.0 </n2spinup>
<maxn1> 103.8 </maxn1>
<maxn2> 99.6 </maxn2>
<augmented> 0 </augmented>
<injected> 0 </injected>
<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 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073
0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900
1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800
</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 0.5440 0.3720 0.2410 0.0000
0.2 1.1710 0.9740 0.6970 0.5160 0.3650 0.2310 0.0000
0.4 1.1500 0.9570 0.6920 0.5260 0.3670 0.2230 0.0000
0.6 1.1810 0.9410 0.7210 0.5460 0.3380 0.1880 0.0000
0.8 1.2290 1.0200 0.7820 0.5370 0.2840 0.1450 0.0000
0.9 1.2580 1.0200 0.7820 0.5020 0.2510 0.0650 0.0000
1.0 1.1810 0.9510 0.7210 0.4210 0.1540 0.0150 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>

59
Engines/pw1133g.xml
View file

@ -1,59 +0,0 @@
<?xml version="1.0"?>
<!--
#########################################
# Copyright (c) it0uchpods Design Group #
#########################################
-->
<turbine_engine name="PW1133G">
<milthrust> 26345 </milthrust>
<bypassratio> 8.1 </bypassratio>
<tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed>
<idlen1> 19.7 </idlen1>
<idlen2> 61.2 </idlen2>
<n1spinup> 0.2 </n1spinup>
<n2spinup> 2.0 </n2spinup>
<maxn1> 103.8 </maxn1>
<maxn2> 99.6 </maxn2>
<augmented> 0 </augmented>
<injected> 0 </injected>
<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 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073
0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900
1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800
</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 0.5440 0.3720 0.2410 0.0000
0.2 1.1710 0.9740 0.6970 0.5160 0.3650 0.2310 0.0000
0.4 1.1500 0.9570 0.6920 0.5260 0.3670 0.2230 0.0000
0.6 1.1810 0.9410 0.7210 0.5460 0.3380 0.1880 0.0000
0.8 1.2290 1.0200 0.7820 0.5370 0.2840 0.1450 0.0000
0.9 1.2580 1.0200 0.7820 0.5020 0.2510 0.0650 0.0000
1.0 1.1810 0.9510 0.7210 0.4210 0.1540 0.0150 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>

59
Engines/v2522_a5.xml
View file

@ -1,59 +0,0 @@
<?xml version="1.0"?>
<!--
#########################################
# Copyright (c) it0uchpods Design Group #
#########################################
-->
<turbine_engine name="V2522_A5">
<milthrust> 26600 </milthrust>
<bypassratio> 8.1 </bypassratio>
<tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed>
<idlen1> 22.4 </idlen1>
<idlen2> 60.9 </idlen2>
<n1spinup> 0.2 </n1spinup>
<n2spinup> 2.0 </n2spinup>
<maxn1> 103.8 </maxn1>
<maxn2> 99.6 </maxn2>
<augmented> 0 </augmented>
<injected> 0 </injected>
<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 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073
0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900
1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800
</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 0.5440 0.3720 0.2410 0.0000
0.2 1.1710 0.9740 0.6970 0.5160 0.3650 0.2310 0.0000
0.4 1.1500 0.9570 0.6920 0.5260 0.3670 0.2230 0.0000
0.6 1.1810 0.9410 0.7210 0.5460 0.3380 0.1880 0.0000
0.8 1.2290 1.0200 0.7820 0.5370 0.2840 0.1450 0.0000
0.9 1.2580 1.0200 0.7820 0.5020 0.2510 0.0650 0.0000
1.0 1.1810 0.9510 0.7210 0.4210 0.1540 0.0150 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>

59
Engines/v2533_a5.xml
View file

@ -1,59 +0,0 @@
<?xml version="1.0"?>
<!--
#########################################
# Copyright (c) it0uchpods Design Group #
#########################################
-->
<turbine_engine name="V2533_A5">
<milthrust> 26600 </milthrust>
<bypassratio> 8.1 </bypassratio>
<tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed>
<idlen1> 22.4 </idlen1>
<idlen2> 60.9 </idlen2>
<n1spinup> 0.2 </n1spinup>
<n2spinup> 2.0 </n2spinup>
<maxn1> 103.8 </maxn1>
<maxn2> 99.6 </maxn2>
<augmented> 0 </augmented>
<injected> 0 </injected>
<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 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073
0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900
1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800
</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 0.5440 0.3720 0.2410 0.0000
0.2 1.1710 0.9740 0.6970 0.5160 0.3650 0.2310 0.0000
0.4 1.1500 0.9570 0.6920 0.5260 0.3670 0.2230 0.0000
0.6 1.1810 0.9410 0.7210 0.5460 0.3380 0.1880 0.0000
0.8 1.2290 1.0200 0.7820 0.5370 0.2840 0.1450 0.0000
0.9 1.2580 1.0200 0.7820 0.5020 0.2510 0.0650 0.0000
1.0 1.1810 0.9510 0.7210 0.4210 0.1540 0.0150 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>

2
revision.txt
View file

@ -1 +1 @@
2141
2142