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CRJ700jsb.xml
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<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<fdm_config name="CRJ700jsb" version="2.0" release="ALPHA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader>
<author> Aeromatic v 3.1.0 </author>
<filecreationdate> 13 Jan 2016 </filecreationdate>
<version>$Revision: 1.49 $</version>
<description> Models a crj2. </description>
</fileheader>
<!--
File: crj2.xml
Inputs:
name: crj2
type: 2 engine transonic transport
stall speed: 110.00kts
max weight: 72750.00 lb
length: 106.00 ft
wing:
span: 76.00 ft
area: 760.00 sq-ft
chord: 8.17 ft
aspect ratio: 9.30:1
taper ratio: 1.00:1
incidence: 2.00 degrees
dihedral: 0.00 degrees
sweep: 0.00 degrees
no. engines: 2
engine type: Turbine Engine
engine layout: aft fuselage
control type: Conventional with Yaw Damper
gear type: tricycle
steering type: steering
retractable?: yes
Outputs:
wing loading: 95.72 lb/sq-ft
payload: 9099.25 lbs
CL-alpha: 5.76 per radian
CL-0: 0.20
CL-max: 2.34
CD-0: 0.02
K: 0.04
Mcrit: 0.53
-->
<metrics>
<wingarea unit="FT2"> 760.00 </wingarea>
<wingspan unit="FT" > 76.00 </wingspan>
<wing_incidence> 2.00 </wing_incidence>
<chord unit="FT" > 8.17 </chord>
<htailarea unit="FT2"> 190.00 </htailarea>
<htailarm unit="FT" > 47.70 </htailarm>
<vtailarea unit="FT2"> 152.00 </vtailarea>
<vtailarm unit="FT" > 47.70 </vtailarm>
<location name="AERORP" unit="IN">
<x> 699.60 </x>
<y> 0.00 </y>
<z> 0.00 </z>
</location>
<location name="EYEPOINT" unit="IN">
<x> 89.04 </x>
<y> -30.00 </y>
<z> 70.00 </z>
</location>
<location name="VRP" unit="IN">
<x> 0.0 </x>
<y> 0.0 </y>
<z> 0.0 </z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 121918.78 </ixx>
<iyy unit="SLUG*FT2"> 547951.75 </iyy>
<izz unit="SLUG*FT2"> 591782.19 </izz>
<emptywt unit="LBS" > 43499.00 </emptywt>
<location name="CG" unit="IN">
<x> 699.60 </x>
<y> 0.00 </y>
<z> -31.80 </z>
</location>
<pointmass name="Payload">
<description> 9099.25 LBS should bring model up to entered max weight </description>
<weight unit="LBS"> 4549.62 </weight>
<location name="POINTMASS" unit="IN">
<x> 699.60 </x>
<y> 0.00 </y>
<z> -31.80 </z>
</location>
</pointmass>
</mass_balance>
<propulsion>
<engine file="cf34-8">
<location unit="IN">
<x> 1212.00 </x>
<y> -20.00 </y>
<z> 0.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
<feed> 0 </feed>
<thruster file="direct">
<sense> 1 </sense>
<location unit="IN">
<x> 1212.00 </x>
<y> -20.00 </y>
<z> 0.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
</thruster>
</engine>
<engine file="cf34-8">
<location unit="IN">
<x> 1212.00 </x>
<y> 20.00 </y>
<z> 0.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
<feed> 1 </feed>
<thruster file="direct">
<sense> 1 </sense>
<location unit="IN">
<x> 1212.00 </x>
<y> 20.00 </y>
<z> 0.00 </z>
</location>
<orient unit="DEG">
<pitch> 0.00 </pitch>
<roll> 0.00 </roll>
<yaw> 0.00 </yaw>
</orient>
</thruster>
</engine>
<tank type="FUEL" number="0">
<location unit="IN">
<x> 699.60 </x>
<y> 0.00 </y>
<z> -31.80 </z>
</location>
<capacity unit="LBS"> 6717.25 </capacity>
<contents unit="LBS"> 3358.62 </contents>
</tank>
<tank type="FUEL" number="1">
<location unit="IN">
<x> 699.60 </x>
<y> 0.00 </y>
<z> -31.80 </z>
</location>
<capacity unit="LBS"> 6717.25 </capacity>
<contents unit="LBS"> 3358.62 </contents>
</tank>
<tank type="FUEL" number="2">
<location unit="IN">
<x> 699.60 </x>
<y> 0.00 </y>
<z> -31.80 </z>
</location>
<capacity unit="LBS"> 6717.25 </capacity>
<contents unit="LBS"> 3358.62 </contents>
</tank>
</propulsion>
<ground_reactions>
<contact type="BOGEY" name="NOSE">
<location unit="IN">
<x> 165.36 </x>
<y> 0.00 </y>
<z> -152.64 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 21825.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 10912.50 </damping_coeff>
<max_steer unit="DEG"> 5.00 </max_steer>
<brake_group> NONE </brake_group>
<retractable> 1 </retractable>
</contact>
<contact type="BOGEY" name="LEFT_MAIN">
<location unit="IN">
<x> 727.58 </x>
<y> -82.08 </y>
<z> -152.64 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 72750.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 36375.00 </damping_coeff>
<max_steer unit="DEG">0</max_steer>
<brake_group> LEFT </brake_group>
<retractable> 1 </retractable>
</contact>
<contact type="BOGEY" name="RIGHT_MAIN">
<location unit="IN">
<x> 727.58 </x>
<y> 82.08 </y>
<z> -152.64 </z>
</location>
<static_friction> 0.80 </static_friction>
<dynamic_friction> 0.50 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
<spring_coeff unit="LBS/FT"> 72750.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 36375.00 </damping_coeff>
<max_steer unit="DEG">0</max_steer>
<brake_group> RIGHT </brake_group>
<retractable> 1 </retractable>
</contact>
<contact type="STRUCTURE" name="LEFT_WING">
<location unit="IN">
<x> 699.60 </x>
<y> -38.00 </y>
<z> -31.80 </z>
</location>
<static_friction> 1 </static_friction>
<dynamic_friction> 1 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 72750.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 72750.00 </damping_coeff>
</contact>
<contact type="STRUCTURE" name="RIGHT_WING">
<location unit="IN">
<x> 699.60 </x>
<y> 38.00 </y>
<z> -31.80 </z>
</location>
<static_friction> 1 </static_friction>
<dynamic_friction> 1 </dynamic_friction>
<spring_coeff unit="LBS/FT"> 72750.00 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 72750.00 </damping_coeff>
</contact>
</ground_reactions>
<system file="Systems/Propulsion.xml"/>
<!--<system file="Thrust Reverse.xml"/>-->
<system file="Systems/Aircraft control.xml"/>
<system file="Systems/Landing Gear.xml"/>
<system file="Systems/Flaps.xml"/>
<system file="Systems/Spoilers.xml"/>
<system file="Systems/Speedbrake.xml"/>
<flight_control name="FCS: crj2">
</flight_control>
<aerodynamics>
<axis name="LIFT">
<function name="aero/force/Lift_alpha">
<description>Lift due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.20 -0.9525
0.00 0.2000
0.37 2.3367
0.60 1.0547
</tableData>
</table>
</product>
</function>
<function name="aero/force/Lift_pitch_rate">
<description>Lift_due_to_pitch_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>velocities/q-aero-rad_sec</property>
<property>aero/ci2vel</property>
<value> 10.9588 </value>
</product>
</function>
<function name="aero/force/Lift_alpha_rate">
<description>Lift_due_to_alpha_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/alphadot-rad_sec</property>
<property>aero/ci2vel</property>
<value> 3.8792 </value>
</product>
</function>
<function name="aero/force/Lift_elevator">
<description>Lift due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/elevator-pos-rad</property>
<value> 0.4269 </value>
</product>
</function>
<function name="aero/force/Lift_flap">
<description>Delta Lift due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.0460 </value>
</product>
</function>
<function name="aero/force/Lift_spoilers">
<description>Delta Lift due to spoilers</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/spoilers-pos-norm</property>
<value> -0.1000 </value>
</product>
</function>
</axis>
<axis name="DRAG">
<function name="aero/force/Drag_basic">
<description>Drag at zero lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-1.57 1.5000
-0.26 0.0260
0.00 0.0200
0.26 0.0260
1.57 1.5000
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_induced">
<description>Induced drag</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/cl-squared</property>
<value> 0.0378 </value>
</product>
</function>
<function name="aero/force/Drag_mach">
<description>Drag due to mach</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.00 0.0000
0.53 0.0000
1.10 0.0230
1.80 0.0150
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_beta">
<description>Drag due to sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/beta-rad</independentVar>
<tableData>
-1.57 1.2300
-0.26 0.0500
0.00 0.0000
0.26 0.0500
1.57 1.2300
</tableData>
</table>
</product>
</function>
<function name="aero/force/Drag_elevator">
<description>Drag due to Elevator Deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<abs><property>fcs/elevator-pos-rad</property></abs>
<value> 0.0400 </value>
</product>
</function>
<function name="aero/force/Drag_gear">
<description>Drag due to gear</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>gear/gear-pos-norm</property>
<value> 0.0150 </value>
</product>
</function>
<function name="aero/force/Drag_flap">
<description>Drag due to flaps</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/flap-pos-deg</property>
<value> 0.0018 </value>
</product>
</function>
<function name="aero/force/Drag_spoilers">
<description>Drag due to spoilers</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/spoilers-pos-norm</property>
<value> 0.0200 </value>
</product>
</function>
<function name="aero/force/Drag_speedbrake">
<description>Drag due to speedbrakes</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/speedbrake-pos-norm</property>
<value> 0.1200 </value>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/force/Side_beta">
<description>Side force due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<value> -0.4619 </value>
</product>
</function>
<function name="aero/force/Side_roll_rate">
<description>Side_force_due_to_roll_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value> -0.0000 </value>
</product>
</function>
<function name="aero/force/Side_yaw_rate">
<description>Side_force_due_to_yaw_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value> 0.5798 </value>
</product>
</function>
<function name="aero/force/Side_rudder">
<description>Side_force_due_to_rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/rudder-pos-rad</property>
<value> 0.2813 </value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/moment/Pitch_alpha">
<description>Pitch moment due to alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<value> -0.6000 </value>
</product>
</function>
<function name="aero/moment/Pitch_elevator">
<description>Pitch moment due to elevator</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>fcs/elevator-pos-rad</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 -1.2000
2.0 -0.3000
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Pitch_damp">
<description>Pitch moment due to pitch rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value> -17.0000 </value>
</product>
</function>
<function name="aero/moment/Pitch_alphadot">
<description>Pitch moment due to alpha rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value> -6.0000 </value>
</product>
</function>
</axis>
<axis name="ROLL">
<function name="aero/moment/Roll_beta">
<description>Roll moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value> -0.1000 </value>
</product>
</function>
<function name="aero/moment/Roll_damp">
<description>Roll moment due to roll rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-aero-rad_sec</property>
<value> -0.8459 </value>
</product>
</function>
<function name="aero/moment/Roll_yaw">
<description>Roll moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value> 0.4178 </value>
</product>
</function>
<function name="aero/moment/Roll_aileron">
<description>Roll moment due to aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 0.1000
2.0 0.0250
</tableData>
</table>
</product>
</function>
<function name="aero/moment/Roll_rudder">
<description>Roll moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value> 0.0100 </value>
</product>
</function>
<function name="aero/moment/Roll_spoilers">
<description>Roll moment due to spoilers</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/spoilers-pos-norm</property>
<property>fcs/left-aileron-pos-rad</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<tableData>
-0.175 0.0000
0.0 0.2400
0.175 0.0000
</tableData>
</table>
</product>
</function>
</axis>
<axis name="YAW">
<function name="aero/moment/Yaw_beta">
<description>Yaw moment due to beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<value> 0.2899 </value>
</product>
</function>
<function name="aero/moment/Yaw_rol_rate">
<description>Yaw_moment_due_to_roll_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/p-rad_sec</property>
<value> -0.0269 </value>
</product>
</function>
<function name="aero/moment/Yaw_damp">
<description>Yaw moment due to yaw rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value> -0.3639 </value>
</product>
</function>
<function name="aero/moment/Yaw_rudder">
<description>Yaw moment due to rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/rudder-pos-rad</property>
<value> -0.1766 </value>
</product>
</function>
<function name="aero/moment/Yaw_aileron">
<description>Adverse yaw</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>fcs/left-aileron-pos-rad</property>
<value> 0.0000 </value>
</product>
</function>
</axis>
</aerodynamics>
<external_reactions>
</external_reactions>
</fdm_config>