Add Frederic Bouvier's A320 model
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ehofman
parent
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2 changed files with 200 additions and 0 deletions
93
Aircraft/A320-jsbsim-set.xml
Executable file
93
Aircraft/A320-jsbsim-set.xml
Executable file
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<?xml version="1.0"?>
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<PropertyList>
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<sim>
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<description>Airbus A320-200</description>
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<flight-model>jsb</flight-model>
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<aero>A320</aero>
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<fuel-fraction>0.5</fuel-fraction>
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<systems>
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<electrical>
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<path>Aircraft/Generic/generic-electrical.xml</path>
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</electrical>
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</systems>
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<sound>
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<audible>true</audible>
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<path>Aircraft/A320/A320-sound.xml</path>
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</sound>
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<!--
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<panel>
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<path>Aircraft/737/Panels/737-trans-mini-panel.xml</path>
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<visibility>true</visibility>
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</panel>
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-->
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<hud>
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<path>Huds/Custom/default.xml</path>
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<visibility>true</visibility>
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</hud>
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<model>
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<path>Aircraft/A320/Models/a320-fb.xml</path>
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</model>
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<view>
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<internal archive="y">true</internal>
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<config>
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<!-- x/y/z == right/up/back -->
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<x-offset-m archive="y">-0.6</x-offset-m>
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<y-offset-m archive="y">3.26</y-offset-m>
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<z-offset-m archive="y">-16.16</z-offset-m>
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<pitch-offset-deg archive="y">-11.0</pitch-offset-deg>
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</config>
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</view>
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<view n="1">
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<config>
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<!-- big plane, so extend chase view offset a bit -->
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<z-offset-m type="double" archive="y">-45.0</z-offset-m>
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</config>
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</view>
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<view n="4">
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<config>
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<!-- big plane, so extend chase view offset a bit -->
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<z-offset-m type="double" archive="y">-45.0</z-offset-m>
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</config>
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</view>
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<!--
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<current-view>
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<pitch-offset-deg archive="y">-11.0</pitch-offset-deg>
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</current-view>
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-->
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</sim>
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<consumables>
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<fuel>
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<tank n="0">
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<level-gal_us archive="y">1500</level-gal_us>
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</tank>
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<tank n="1">
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<level-gal_us archive="y">1500</level-gal_us>
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</tank>
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</fuel>
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</consumables>
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<autopilot>
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<config>
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<min-climb-speed-kt type="float">150.0</min-climb-speed-kt>
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<best-climb-speed-kt type="float">300.0</best-climb-speed-kt>
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<target-climb-rate-fpm type="float">2000.0</target-climb-rate-fpm>
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<target-descent-rate-fpm type="float">1500.0</target-descent-rate-fpm>
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<elevator-adj-factor type="float">3500.0</elevator-adj-factor>
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<integral-contribution type="float">0.01</integral-contribution>
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<zero-pitch-throttle type="float">0.0001</zero-pitch-throttle>
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<zero-pitch-trim-full-throttle type="float">0.0001</zero-pitch-trim-full-throttle>
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<max-roll-deg type="float">30</max-roll-deg>
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<max-aileron type="float">1.0</max-aileron>
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</config>
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</autopilot>
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</PropertyList>
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107
Engine/CFM56_5_sim.xml
Executable file
107
Engine/CFM56_5_sim.xml
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<?xml version="1.0"?>
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<!-- CFM56-5 turbofan engine model
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Version 1.0, 4 Jun 2003, David Culp, davidculp2@attbi.com
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-->
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<FG_SIMTURBINE NAME="CFM56_5">
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<!--
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MAXMILTHRUST max static thrust at S.L. (installed), lbf
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BYPASSRATIO bypass ratio
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TSFC thrust-specific fuel consumption (lbm/hr/lbf)
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ATSFC augmented TSFC (lbm/hr/lbf)
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IDLEN1 idle percent rpm of fan spool
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IDLEN2 idle percent rpm of inner spool
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MAXN1 N1 at 100% throttle
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MAXN2 N2 at 100% throttle
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AUGMENTED =1 if augmentation installed, else =0
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INJECTED =1 if water injection installed, else =0
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TABLE(0) idle thrust vs. altitude and mach
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TABLE(1) maximum un-augmented thrust vs. altitude and mach
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TABLE(2) augmented thrust multiplier vs. altitude and mach
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TABLE(3) water-injection multiplier vs. altitude and mach
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-->
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MAXMILTHRUST 25000
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BYPASSRATIO 5.9
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TSFC 0.657
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ATSFC 0.0
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IDLEN1 30.0
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IDLEN2 60.0
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MAXN1 100.0
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MAXN2 100.0
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AUGMENTED 0
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INJECTED 0
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<TABLE NAME="IdleThrust" TYPE="TABLE">
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Idle_power_thrust_factor
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6
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6
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 0.0836 0.0528 0.0694 0.0899 0.1183 0.1467
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0.2 0.0501 0.0335 0.0544 0.0797 0.1049 0.1341
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0.4 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
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0.6 -0.0804 -0.0560 -0.0237 0.0276 0.0718 0.1073
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0.8 -0.2129 -0.1498 -0.1025 -0.0195 0.0473 0.0868
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1.0 -0.2839 -0.1104 -0.0469 -0.0270 -0.0158 0.0552
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</TABLE>
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<TABLE NAME="MilThrust" TYPE="TABLE">
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Effects_of_altitude_and_mach_on_thrust
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7
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6
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 1.0000 0.7216 0.4890 0.3115 0.1932 0.1104
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0.2 1.0000 0.7216 0.4979 0.3186 0.1948 0.1104
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0.4 0.9945 0.7344 0.5213 0.3383 0.2050 0.1230
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0.6 0.9968 0.7759 0.5591 0.3675 0.2240 0.1309
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0.8 0.9771 0.8025 0.6112 0.4196 0.2563 0.1522
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0.9 0.9300 0.7900 0.6000 0.3900 0.2300 0.1300
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1.0 0.5000 0.5000 0.4000 0.2000 0.1500 0.0900
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</TABLE>
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<TABLE NAME="AugThrust" TYPE="TABLE">
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Augmented_thrust_factor
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8
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6
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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0.2 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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0.4 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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0.6 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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0.8 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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1.0 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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1.2 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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1.4 1.4146 1.4146 1.4146 1.4146 1.4146 1.4146
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</TABLE>
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<TABLE NAME="WaterFactor" TYPE="TABLE">
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Water_Injection_factor
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8
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6
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velocities/mach-norm
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position/h-sl-ft
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none
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0 10000 20000 30000 40000 50000
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0.0 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.2 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.4 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.6 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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0.8 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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1.0 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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1.2 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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1.4 1.2000 1.2000 1.2000 1.2000 1.2000 1.2000
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</TABLE>
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</FG_SIMTURBINE>
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