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Add Frederic Bouvier's A320 model

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ehofman 2003-06-22 08:22:17 +00:00
parent c18a2b580a
commit 249fe3fccb
2 changed files with 200 additions and 0 deletions
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93
Aircraft/A320-jsbsim-set.xml Executable file
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<?xml version="1.0"?>
<PropertyList>
<sim>
<description>Airbus A320-200</description>
<flight-model>jsb</flight-model>
<aero>A320</aero>
<fuel-fraction>0.5</fuel-fraction>
<systems>
<electrical>
<path>Aircraft/Generic/generic-electrical.xml</path>
</electrical>
</systems>
<sound>
<audible>true</audible>
<path>Aircraft/A320/A320-sound.xml</path>
</sound>
<!--
<panel>
<path>Aircraft/737/Panels/737-trans-mini-panel.xml</path>
<visibility>true</visibility>
</panel>
-->
<hud>
<path>Huds/Custom/default.xml</path>
<visibility>true</visibility>
</hud>
<model>
<path>Aircraft/A320/Models/a320-fb.xml</path>
</model>
<view>
<internal archive="y">true</internal>
<config>
<!-- x/y/z == right/up/back -->
<x-offset-m archive="y">-0.6</x-offset-m>
<y-offset-m archive="y">3.26</y-offset-m>
<z-offset-m archive="y">-16.16</z-offset-m>
<pitch-offset-deg archive="y">-11.0</pitch-offset-deg>
</config>
</view>
<view n="1">
<config>
<!-- big plane, so extend chase view offset a bit -->
<z-offset-m type="double" archive="y">-45.0</z-offset-m>
</config>
</view>
<view n="4">
<config>
<!-- big plane, so extend chase view offset a bit -->
<z-offset-m type="double" archive="y">-45.0</z-offset-m>
</config>
</view>
<!--
<current-view>
<pitch-offset-deg archive="y">-11.0</pitch-offset-deg>
</current-view>
-->
</sim>
<consumables>
<fuel>
<tank n="0">
<level-gal_us archive="y">1500</level-gal_us>
</tank>
<tank n="1">
<level-gal_us archive="y">1500</level-gal_us>
</tank>
</fuel>
</consumables>
<autopilot>
<config>
<min-climb-speed-kt type="float">150.0</min-climb-speed-kt>
<best-climb-speed-kt type="float">300.0</best-climb-speed-kt>
<target-climb-rate-fpm type="float">2000.0</target-climb-rate-fpm>
<target-descent-rate-fpm type="float">1500.0</target-descent-rate-fpm>
<elevator-adj-factor type="float">3500.0</elevator-adj-factor>
<integral-contribution type="float">0.01</integral-contribution>
<zero-pitch-throttle type="float">0.0001</zero-pitch-throttle>
<zero-pitch-trim-full-throttle type="float">0.0001</zero-pitch-trim-full-throttle>
<max-roll-deg type="float">30</max-roll-deg>
<max-aileron type="float">1.0</max-aileron>
</config>
</autopilot>
</PropertyList>

107
Engine/CFM56_5_sim.xml Executable file
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<?xml version="1.0"?>
<!-- CFM56-5 turbofan engine model
Version 1.0, 4 Jun 2003, David Culp, davidculp2@attbi.com
-->
<FG_SIMTURBINE NAME="CFM56_5">
<!--
MAXMILTHRUST max static thrust at S.L. (installed), lbf
BYPASSRATIO bypass ratio
TSFC thrust-specific fuel consumption (lbm/hr/lbf)
ATSFC augmented TSFC (lbm/hr/lbf)
IDLEN1 idle percent rpm of fan spool
IDLEN2 idle percent rpm of inner spool
MAXN1 N1 at 100% throttle
MAXN2 N2 at 100% throttle
AUGMENTED =1 if augmentation installed, else =0
INJECTED =1 if water injection installed, else =0
TABLE(0) idle thrust vs. altitude and mach
TABLE(1) maximum un-augmented thrust vs. altitude and mach
TABLE(2) augmented thrust multiplier vs. altitude and mach
TABLE(3) water-injection multiplier vs. altitude and mach
-->
MAXMILTHRUST 25000
BYPASSRATIO 5.9
TSFC 0.657
ATSFC 0.0
IDLEN1 30.0
IDLEN2 60.0
MAXN1 100.0
MAXN2 100.0
AUGMENTED 0
INJECTED 0
<TABLE NAME="IdleThrust" TYPE="TABLE">
Idle_power_thrust_factor
6
6
velocities/mach-norm
position/h-sl-ft
none
0 10000 20000 30000 40000 50000
0.0 0.0836 0.0528 0.0694 0.0899 0.1183 0.1467
0.2 0.0501 0.0335 0.0544 0.0797 0.1049 0.1341
0.4 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
0.6 -0.0804 -0.0560 -0.0237 0.0276 0.0718 0.1073
0.8 -0.2129 -0.1498 -0.1025 -0.0195 0.0473 0.0868
1.0 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158 0.0552
</TABLE>
<TABLE NAME="MilThrust" TYPE="TABLE">
Effects_of_altitude_and_mach_on_thrust
7
6
velocities/mach-norm
position/h-sl-ft
none
0 10000 20000 30000 40000 50000
0.0 1.0000 0.7216 0.4890 0.3115 0.1932 0.1104
0.2 1.0000 0.7216 0.4979 0.3186 0.1948 0.1104
0.4 0.9945 0.7344 0.5213 0.3383 0.2050 0.1230
0.6 0.9968 0.7759 0.5591 0.3675 0.2240 0.1309
0.8 0.9771 0.8025 0.6112 0.4196 0.2563 0.1522
0.9 0.9300 0.7900 0.6000 0.3900 0.2300 0.1300
1.0 0.5000 0.5000 0.4000 0.2000 0.1500 0.0900
</TABLE>
<TABLE NAME="AugThrust" TYPE="TABLE">
Augmented_thrust_factor
8
6
velocities/mach-norm
position/h-sl-ft
none
0 10000 20000 30000 40000 50000
0.0 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
0.2 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
0.4 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
0.6 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
0.8 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
1.0 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
1.2 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
1.4 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
</TABLE>
<TABLE NAME="WaterFactor" TYPE="TABLE">
Water_Injection_factor
8
6
velocities/mach-norm
position/h-sl-ft
none
0 10000 20000 30000 40000 50000
0.0 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
0.2 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
0.4 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
0.6 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
0.8 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
1.0 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
1.2 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
1.4 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
</TABLE>
</FG_SIMTURBINE>