Engine: New dynamic spoolup/down values, REQUIRES 2018.1.0 or later
This commit is contained in:
Joshua Davidson
parent
adee621c1f
commit
5fe4e3b900
23 changed files with 1194 additions and 309 deletions
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@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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</ground_reactions>
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<propulsion>
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<engine file="cfm56_5a1">
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<engine file="cfm56_5a1_1">
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<location unit="M">
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<x> 14.3962788 </x>
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<y> -5.755 </y>
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@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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</thruster>
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</engine>
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<engine file="cfm56_5a1">
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<engine file="cfm56_5a1_2">
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<location unit="M">
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<x> 14.3962788 </x>
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<y> 5.755 </y>
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@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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</ground_reactions>
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<propulsion>
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<engine file="cfm56_5b4">
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<engine file="cfm56_5b4_1">
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<location unit="M">
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<x> 14.3962788 </x>
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<y> -5.755 </y>
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@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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</thruster>
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</engine>
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<engine file="cfm56_5b4">
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<engine file="cfm56_5b4_2">
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<location unit="M">
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<x> 14.3962788 </x>
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<y> 5.755 </y>
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@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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</ground_reactions>
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<propulsion>
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<engine file="v2527_a5">
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<engine file="v2527_a5_1">
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<location unit="M">
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<x> 14.3962788 </x>
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<y> -5.755 </y>
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@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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</thruster>
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</engine>
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<engine file="v2527_a5">
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<engine file="v2527_a5_2">
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<location unit="M">
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<x> 14.3962788 </x>
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<y> 5.755 </y>
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@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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</ground_reactions>
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<propulsion>
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<engine file="leap1a26">
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<engine file="leap1a26_1">
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<location unit="M">
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<x> 14.3962788 </x>
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<y> -5.755 </y>
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@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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</thruster>
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</engine>
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<engine file="leap1a26">
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<engine file="leap1a26_2">
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<location unit="M">
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<x> 14.3962788 </x>
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<y> 5.755 </y>
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@ -334,7 +334,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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</ground_reactions>
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<propulsion>
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<engine file="pw1127g">
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<engine file="pw1127g_1">
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<location unit="M">
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<x> 14.3962788 </x>
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<y> -5.755 </y>
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@ -360,7 +360,7 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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</thruster>
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</engine>
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<engine file="pw1127g">
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<engine file="pw1127g_2">
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<location unit="M">
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<x> 14.3962788 </x>
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<y> 5.755 </y>
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@ -126,9 +126,9 @@ setlistener("/systems/acconfig/new-revision", func {
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});
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var mismatch_chk = func {
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if (num(string.replace(getprop("/sim/version/flightgear"),".","")) < 201730) {
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if (num(string.replace(getprop("/sim/version/flightgear"),".","")) < 201810) {
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setprop("/systems/acconfig/mismatch-code", "0x121");
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setprop("/systems/acconfig/mismatch-reason", "FGFS version is too old! Please update FlightGear to at least 2017.3.0.");
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setprop("/systems/acconfig/mismatch-reason", "FGFS version is too old! Please update FlightGear to at least 2018.1.0.");
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if (getprop("/systems/acconfig/out-of-date") != 1) {
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error_mismatch.open();
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}
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@ -1,59 +0,0 @@
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<?xml version="1.0"?>
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<!--
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##############################################
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# Copyright (c) Joshua Davidson (it0uchpods) #
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##############################################
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-->
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<turbine_engine name="CFM56_5A1">
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<milthrust> 25000 </milthrust>
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<bypassratio> 8.1 </bypassratio>
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<tsfc> 0.5 </tsfc>
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<bleed> 0.03 </bleed>
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<idlen1> 19.7 </idlen1>
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<idlen2> 61.2 </idlen2>
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<n1spinup> 0.2 </n1spinup>
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<n2spinup> 1.0 </n2spinup>
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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="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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118
Engines/cfm56_5a1_1.xml
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118
Engines/cfm56_5a1_1.xml
Normal file
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@ -0,0 +1,118 @@
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<?xml version="1.0"?>
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<!--
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##############################################
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# Copyright (c) Joshua Davidson (it0uchpods) #
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##############################################
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-->
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<turbine_engine name="CFM56_5A1">
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<milthrust> 25000 </milthrust>
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<tsfc> 0.5 </tsfc>
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<bleed> 0.03 </bleed>
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<idlen1> 19.7 </idlen1>
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<idlen2> 61.2 </idlen2>
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<n1spinup> 0.2 </n1spinup>
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<n2spinup> 1.0 </n2spinup>
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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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118
Engines/cfm56_5a1_2.xml
Normal file
118
Engines/cfm56_5a1_2.xml
Normal file
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@ -0,0 +1,118 @@
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<?xml version="1.0"?>
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<!--
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##############################################
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# Copyright (c) Joshua Davidson (it0uchpods) #
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##############################################
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-->
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<turbine_engine name="CFM56_5A1">
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<milthrust> 25000 </milthrust>
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<tsfc> 0.5 </tsfc>
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<bleed> 0.03 </bleed>
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<idlen1> 19.7 </idlen1>
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<idlen2> 61.2 </idlen2>
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<n1spinup> 0.2 </n1spinup>
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<n2spinup> 1.0 </n2spinup>
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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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@ -1,59 +0,0 @@
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<?xml version="1.0"?>
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<!--
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##############################################
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# Copyright (c) Joshua Davidson (it0uchpods) #
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##############################################
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-->
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<turbine_engine name="CFM56_5B4">
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<milthrust> 27000 </milthrust>
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<bypassratio> 8.1 </bypassratio>
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<tsfc> 0.5 </tsfc>
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<bleed> 0.03 </bleed>
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<idlen1> 19.7 </idlen1>
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||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </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 0.0458 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>
|
||||
118
Engines/cfm56_5b4_1.xml
Normal file
118
Engines/cfm56_5b4_1.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="CFM56_5B4">
|
||||
|
||||
<milthrust> 27000 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<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>
|
||||
118
Engines/cfm56_5b4_2.xml
Normal file
118
Engines/cfm56_5b4_2.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="CFM56_5B4">
|
||||
|
||||
<milthrust> 27000 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/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[1]/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[1]/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[1]/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>
|
||||
|
|
@ -1,59 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="LEAP1A26">
|
||||
|
||||
<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> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </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 0.0458 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>
|
||||
118
Engines/leap1a26_1.xml
Normal file
118
Engines/leap1a26_1.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="LEAP1A26">
|
||||
|
||||
<milthrust> 27000 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<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>
|
||||
118
Engines/leap1a26_2.xml
Normal file
118
Engines/leap1a26_2.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="LEAP1A26">
|
||||
|
||||
<milthrust> 27000 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/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[1]/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[1]/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[1]/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>
|
||||
|
|
@ -1,59 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="PW1127G">
|
||||
|
||||
<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> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </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 0.0458 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>
|
||||
118
Engines/pw1127g_1.xml
Normal file
118
Engines/pw1127g_1.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="PW1127G">
|
||||
|
||||
<milthrust> 26345 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<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>
|
||||
118
Engines/pw1127g_2.xml
Normal file
118
Engines/pw1127g_2.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="PW1127G">
|
||||
|
||||
<milthrust> 26345 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 19.7 </idlen1>
|
||||
<idlen2> 61.2 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/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[1]/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[1]/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[1]/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>
|
||||
|
|
@ -1,59 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="V2527_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> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </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 0.0458 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>
|
||||
118
Engines/v2527_a5_1.xml
Normal file
118
Engines/v2527_a5_1.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="V2527_A5">
|
||||
|
||||
<milthrust> 26600 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 22.4 </idlen1>
|
||||
<idlen2> 60.9 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<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>
|
||||
118
Engines/v2527_a5_2.xml
Normal file
118
Engines/v2527_a5_2.xml
Normal file
|
|
@ -0,0 +1,118 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
##############################################
|
||||
# Copyright (c) Joshua Davidson (it0uchpods) #
|
||||
##############################################
|
||||
-->
|
||||
|
||||
<turbine_engine name="V2527_A5">
|
||||
|
||||
<milthrust> 26600 </milthrust>
|
||||
<tsfc> 0.5 </tsfc>
|
||||
<bleed> 0.03 </bleed>
|
||||
<idlen1> 22.4 </idlen1>
|
||||
<idlen2> 60.9 </idlen2>
|
||||
<n1spinup> 0.2 </n1spinup>
|
||||
<n2spinup> 1.0 </n2spinup>
|
||||
<maxn1> 103.8 </maxn1>
|
||||
<maxn2> 101.4 </maxn2>
|
||||
<augmented> 0 </augmented>
|
||||
<injected> 0 </injected>
|
||||
|
||||
<function name="N1SpoolUp">
|
||||
<table>
|
||||
<independentVar lookup="row">/engines/engine[1]/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[1]/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[1]/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[1]/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>
|
||||
|
|
@ -1,7 +1,7 @@
|
|||
# INSTALL
|
||||
## Prerequisites
|
||||
Have at least following versions installed:
|
||||
* FlightGear 2017.3.0 or newer
|
||||
* FlightGear 2018.1.0 or newer
|
||||
|
||||
## Install using ZIP Snapshot
|
||||
[Download](https://github.com/it0uchpods/IDG-A32X/archive/master.zip) the zip file.
|
||||
|
|
|
|||
|
|
@ -1 +1 @@
|
|||
4416
|
||||
4500
|
||||
Reference in a new issue