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dh106-yasim.xml
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dh106-yasim.xml
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<?xml version="1.0" encoding="UTF-8"?>
<!-- de Havilland DH 106 Comet 4 : 2011 BARANGER Emmanuel
Source : http://en.wikipedia.org/wiki/De_Havilland_Comet
wingspan : 35.00 m ( 114 ft 10 in )
length : 33.99 m ( 111 ft 6 in )
height : 8.99 m ( 29 ft 6 in )
Moteurs : 4 Rolls-Royce Spey turbofans ( 12160 lbf each )
Empty weight : 75400 lb ( 34200 kg )
Cruise speed : 846 km/h ( 457 kt )
-->
<airplane mass="75400">
<!-- Approach configuration -->
<approach speed="120" aoa="5" fuel="0.37">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.2"/>
<control-setting axis="/controls/engines/engine[2]/throttle" value="0.2"/>
<control-setting axis="/controls/engines/engine[3]/throttle" value="0.2"/>
<control-setting axis="/controls/engines/engine[0]/reheat" value="0"/>
<control-setting axis="/controls/engines/engine[1]/reheat" value="0"/>
<control-setting axis="/controls/engines/engine[2]/reheat" value="0"/>
<control-setting axis="/controls/engines/engine[3]/reheat" value="0"/>
<control-setting axis="/controls/flight/flaps" value="0.5"/>
<control-setting axis="/surface-positions/flap-pos-norm" value="0.5"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="429" alt="44000" fuel="0.7">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.75"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.75"/>
<control-setting axis="/controls/engines/engine[2]/throttle" value="0.75"/>
<control-setting axis="/controls/engines/engine[3]/throttle" value="0.75"/>
<control-setting axis="/controls/engines/engine[0]/reheat" value="0"/>
<control-setting axis="/controls/engines/engine[1]/reheat" value="0"/>
<control-setting axis="/controls/engines/engine[2]/reheat" value="0"/>
<control-setting axis="/controls/engines/engine[3]/reheat" value="0"/>
<control-setting axis="/controls/flight/flaps" value="0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
</cruise>
<cockpit x="16.600" y="0.438" z="-0.710"/>
<!-- fuselage -->
<fuselage ax="18.169" ay=" 0.000" az="-1.521" bx=" 12.463" by=" 0.000" bz="-1.1375" width="3.336" taper="0.22" midpoint="1"/>
<fuselage ax="12.463" ay=" 0.000" az="-1.1375" bx="-4.831" by="0.000" bz="-1.1146" width="3.348" taper="1.0" midpoint="0.5" cy="47.0" cz="47.0"/>
<fuselage ax="-4.831" ay=" 0.000" az="-1.1146" bx="-15.6745" by=" 0.000" bz="0.5606" width="3.348" taper="0.21" midpoint="0" cy="34.4" cz="34.4"/>
<!-- Engines left -->
<fuselage ax=" 4.824" ay=" 3.673" az="-2.372" bx=" -4.497" by="2.875" bz="-2.388" width="1.1900" taper="0.9" midpoint="0" cy="2.4" cz="6"/>
<fuselage ax=" 5.467" ay=" 2.158" az="-2.38" bx=" -4.74" by=" 2.885" bz="-2.388" width="1.1900" taper="0.9" midpoint="0" cy="2.4" cz="6"/>
<!-- Engines right -->
<fuselage ax=" 5.467" ay="-2.158" az="-2.38" bx=" -4.74" by="-2.885" bz="-2.388" width="1.1900" taper="0.9" midpoint="0" cy="2.4" cz="6"/>
<fuselage ax=" 4.824" ay="-3.673" az="-2.372" bx=" -4.497" by="-2.875" bz="-2.388" width="1.1900" taper="0.9" midpoint="0" cy="2.4" cz="6"/>
<!-- Wing tanks -->
<!-- Left tank -->
<fuselage ax="-3.5233" ay="12.4301" az="-2.095" bx="-0.0297" by="12.4301" bz="-0.0949"
width="1.185" taper="0.3" midpoint="0.53" />
<!-- Right tank -->
<fuselage ax="-3.5233" ay="-12.4301" az="-2.095" bx="-0.0297" by="-12.4301" bz="-0.0949"
width="1.185" taper="0.3" midpoint="0.53" />
<wing x="1.512" y="1.67" z="-2.494"
chord="8.805"
length="17"
taper="0.30"
incidence="1.2"
twist="-0.9"
sweep="15"
dihedral="3"
camber="0.04">
<stall aoa="18" width="6" peak="3"/>
<flap0 start="0.05" end="0.64" lift="1.6" drag="1.8"/>
<flap1 start="0.64" end="1" lift="1.3" drag="1.1"/>
<slat start="0" end="1" aoa="5" drag="1.2"/>
<spoiler start="0.35" end="0.50" lift="0.3" drag="3.0"/>
<control-input axis="/controls/flight/spoilers" control="SPOILER"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-input axis="/surface-positions/flap-pos-norm" control="SLAT"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<control-output control="SPOILER" prop="/surface-positions/speedbrake-pos-norm"/>
<control-output control="FLAP0" prop="/surface-positions/flaps-pos-norm"/>
<control-output control="FLAP0" prop="/surface-positions/slats"/>
<control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-pos-norm"/>
<control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-pos-norm"/>
<control-speed control="FLAP0" transition-time="10"/>
<control-speed control="SPOILER" transition-time="5"/>
</wing>
<hstab x="-13.584" y="0" z="-0.481"
chord="3.749"
length="7.235"
taper="0.46"
effectiveness="1.48"
camber="0.01"
sweep="5"
dihedral="10">
<stall aoa="20" width="5" peak="2.5"/>
<flap0 start="0" end="1" lift="1.35" drag="1.1"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab>
<vstab x="-13.900" y="0.00" z="-0.669"
chord="3.752"
length="5.230"
taper="0.30"
sweep="0">
<stall aoa="22" width="7" peak="3.5"/>
<flap0 start="0" end="1" lift="1.3" drag="1.1"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm" min="1" max="-1"/>
</vstab>
<!-- Engines source : http://en.wikipedia.org/wiki/Rolls-Royce_Avon
name : Rolls-Royce Avon
type : Turbojet
power cruise : 12690 lbf dry/16360 lbf with reheat
weight : 2890 lb (1310 kg)
-->
<!-- Exterior left -->
<jet x="2.699" y="3.517" z="-2.364"
mass="2890"
thrust="12690"
afterburner="16360"
tsfc="0.60"
epr="5.66">
<actionpt x="-4.497" y="3.875" z="-2.388"/>
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/reheat" control="REHEAT"/>
</jet>
<!-- Interior left -->
<jet x="2.699" y="2.082" z="-2.364"
mass="2890"
thrust="12690"
afterburner="16360"
tsfc="0.60"
epr="5.66">
<actionpt x="-3.818" y="2.880" z="-2.388"/>
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/reheat" control="REHEAT"/>
</jet>
<!-- Interior right -->
<jet x="2.699" y="-2.082" z="-2.364"
mass="2890"
thrust="12690"
afterburner="16360"
tsfc="0.60"
epr="5.66">
<actionpt x="-4.652" y="-2.880" z="-2.388"/>
<control-input axis="/controls/engines/engine[2]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[2]/reheat" control="REHEAT"/>
</jet>
<!-- Exterior right -->
<jet x="2.699" y="-3.517" z="-2.364"
mass="2890"
thrust="12690"
afterburner="16360"
tsfc="0.60"
epr="5.66">
<actionpt x="-4.497" y="-3.875" z="-2.388"/>
<control-input axis="/controls/engines/engine[3]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[3]/reheat" control="REHEAT"/>
</jet>
<!-- nose -->
<gear x="15.733" y="0.00" z="-4.437"
compression="0.75"
spring="0.7"
damp="4">
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<gear x="0.346" y="4.120" z="-4.517"
compression="1.1"
spring="1.8">
<control-input axis="/controls/gear/brake-left" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<gear x="0.346" y="-4.120" z="-4.517"
compression="1.1"
spring="1.8">
<control-input axis="/controls/gear/brake-right" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<!-- landing gear aero drag right -->
<vstab x="15.733" y="0.00" z="-2.837"
taper="1"
incidence="0"
twist="0"
chord="0.274"
sweep="0"
camber="0.0"
dihedral="0"
length="1.3">
<stall aoa="30"
width="18"
peak="5.5"/>
<flap0 start="0.00"
end="1"
lift="-0.19"
drag="3.06"/>
<control-input axis="/controls/gear/gear-down"
control="FLAP0"/>
<control-output control="FLAP0"
prop="/gear/gear[2]/position-norm"/>
<control-speed control="FLAP0"
transition-time="7" />
</vstab>
<!-- landing gear aero drag left -->
<vstab x="0.346" y="4.120" z="-2.817"
taper="1"
incidence="0"
twist="0"
chord="0.274"
sweep="0"
camber="0.0"
dihedral="0"
length="1.3">
<stall aoa="30"
width="18"
peak="5.5"/>
<flap0 start="0.00"
end="1"
lift="-0.19"
drag="3.06"/>
<control-input axis="/controls/gear/gear-down"
control="FLAP0"/>
<control-output control="FLAP0"
prop="/gear/gear[1]/position-norm"/>
<control-speed control="FLAP0"
transition-time="7" />
</vstab>
<!-- Nose gear aero drag -->
<vstab x="0.346" y="-4.120" z="-2.817"
taper="1"
incidence="0"
twist="0"
chord="0.184"
sweep="0"
camber="0.0"
dihedral="0"
length="1.093">
<stall aoa="30"
width="18"
peak="5.5"/>
<flap0 start="0.00"
end="1"
lift="0.10"
drag="2.86"/>
<control-input axis="/controls/gear/gear-down"
control="FLAP0"/>
<control-output control="FLAP0"
prop="/gear/gear[0]/position-norm"/>
<control-speed control="FLAP0"
transition-time="7" />
</vstab>
<tank x="1.86" y=" 0" z="-2.7" jet="true" capacity="21900"/>
<tank x="1.26" y=" 5.90" z="-2.32" jet="true" capacity="21900"/>
<tank x="1.26" y="-5.90" z="-2.32" jet="true" capacity="21900"/>
<tank x="1.665" y=" 12.4301" z="-0.0949" jet="true" capacity="3500"/>
<tank x="1.665" y="-12.4301" z="-0.0949" jet="true" capacity="3500"/>
<ballast x="10" y="0" z="-2" mass="8000"/>
</airplane>