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citationX-yasim.xml
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citationX-yasim.xml
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<?xml version="1.0" encoding="UTF-8"?>
<!--
Syd Adams
Cessna CE-750 Citation X
Max Cruise M=0.92 -37,000 ft @ 30,000lbs
Airspeed Limits Vmo 600 KIAS Mmo 0.92
Engine Rolls Royce AE3007C1:
TO thrust 6,764 lbs
Bypass ratio 5.1
Press. Ratio 23:1
1586 lbs dry weight
FFlow 0.3222 kg/s 100% pwr takeoff (1278 lbs/hr per engine)
Vmca 110 KIAS 15 degree flap
Vmcl App 5 flap = 129 KIAS
15 flap = 120
Lnd 15 flap = 118
full flap = 108
Wingspan 19.4 m
Wing area 50 m2
tailplane span 7.9m
Sweep 37 degrees
dihedral 2 degrees
Fuel 12938 lbs jet
-->
<airplane mass="21700" version="YASIM_VERSION_CURRENT">
<approach speed="110" aoa="6" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.35"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.35"/>
<control-setting axis="/controls/flight/flaps" value="1"/>
<control-setting axis="/controls/flight/slats" value="1"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
</approach>
<cruise speed="515" alt="41000" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.90"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.90"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<control-setting axis="/surface-positions/flap-pos-norm" value="0"/>
<control-setting axis="/surface-positions/slat-pos-norm" value="0"/>
<control-setting axis="/gear/gear[0]/position-norm" value="0"/>
<control-setting axis="/gear/gear[1]/position-norm" value="0"/>
<control-setting axis="/gear/gear[2]/position-norm" value="0"/>
</cruise>
<cockpit x="7.13" y="0.35" z="0.35"/>
<fuselage ax="10.16" ay="0" az="-0.588" bx="6.87" by="0" bz="0"
width="1.8" taper="0.2" midpoint="1.0" idrag="1.1"/><!--nose-->
<fuselage ax="6.87" ay="0" az="0.0" bx="-1.45" by="0" bz="0"
width="1.8" taper="1.0" midpoint="0.5" idrag="1.1"/><!--fuselage-->
<fuselage ax="-1.45" ay="0" az="0.0" bx="-7.622" by="0" bz="0.37"
width="1.8" taper="0.2" midpoint="0.0" idrag="1.1"/><!--tail-->
<fuselage ax="6.85" ay="0" az="-0.56" bx="-4.18" by="0" bz="-0.56"
width="1.8" taper="0.5" midpoint="0.3" idrag="1.1"/><!--belly-->
<fuselage ax="0.748" ay="1.7" az="0.6" bx="-5.38" by="1.7" bz="0.6"
width="1.4" taper="0.7" midpoint="0.2" idrag="1.1"/><!--LH engine-->
<fuselage ax="0.748" ay="-1.7" az="0.6" bx="-5.38" by="-1.7" bz="0.6"
width="1.4" taper="0.7" midpoint="0.2" idrag="1.1"/><!--RH engine-->
<wing x="1.40" y="0.90" z="-1.0" length="10.8" chord="3.8"
sweep="34.4" dihedral="2.8" taper="0.22" camber="0.0" incidence="1.5" idrag="1.2">
<!--origin : s="33", d="2", t="0.0822",c="0.0", no incidence -->
<stall aoa="15" width="10" peak="1.5"/>
<flap0 start="0" end=".67" lift="1.5" drag="1.6"/>
<flap1 start=".688" end=".858" lift="1.3" drag="1.4"/>
<slat start=".2" end=".8" aoa="3" drag="1.0"/>
<spoiler start=".309" end=".48" lift="1.0" drag="6.0"/>
<control-input axis="/surface-positions/flap-pos-norm" control="FLAP0"/>
<control-input axis="/surface-positions/aileron-pos-norm" control="FLAP1" split="true"/>
<control-input axis="/surface-positions/slat-pos-norm" control="SLAT"/>
<control-input axis="/surface-positions/speedbrake-pos-norm" control="SPOILER"/>
</wing>
<hstab x="-8.562" y="0.15" z="2.98" length="4.85" chord="2.1"
sweep="37" taper="0.3" dihedral="1.4" camber="0" effectiveness="1.5">
<stall aoa="18" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
<!-- controls/elevator/trim is hardcoded in yasim sources -->
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-input axis="/surface-positions/yasim-elevator-minus-trim" control="FLAP0"/>
</hstab>
<vstab x="-6.0" y="0.0" z="0.61" length="4.50" chord="3.2"
sweep="46" taper="0.8">
<stall aoa="14" width="3" peak="1.5"/>
<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
<control-input axis="/surface-positions/rudder-pos-norm" control="FLAP0" invert="true"/>
</vstab>
<!-- Engine mounts -->
<mstab x="-2.5" y="0.8" z="0.72" length="1.0" chord="3.0" incidence="2.0">
</mstab>
<!-- gear drag -->
<mstab x="-1.5" y="1.7" z="-1.0" length="0.3" chord="0.5">
<flap0 start="0" end="1" lift="0" drag="6"/>
<control-input axis="/gear/gear[0]/position-norm" control="FLAP0"/>
</mstab>
<!-- cabin door -->
<vstab x="0" y="0" z="-1.0" length="0.01" chord="0.01">
<flap0 start="0" end="1" lift="0" drag="1"/>
<control-input axis="controls/cabin-door/open" control="FLAP0"/>
<control-output control="FLAP0" prop="/controls/cabin-door/position-norm"/>
<control-speed control="FLAP0" transition-time="3"/>
</vstab>
<!-- apu -->
<vstab x="-6" y="0" z="0.5" length="0.01" chord="0.01">
<flap0 start="0" end="1" lift="0" drag="0"/>
<control-input axis="/controls/APU/running" control="FLAP0"/>
<control-output control="FLAP0" prop="controls/APU/rpm"/>
<control-speed control="FLAP0" transition-time="30"/>
</vstab>
<!-- Total fuel = 13000 lbs -->
<tank x="0.7" y="1.0" z="-0.9" capacity="3510" jet="true"/>
<tank x="0.7" y="-1.0" z="-0.9" capacity="3510" jet="true"/>
<tank x="0.8" y="0.0" z="-1.2" capacity="2990" jet="true"/>
<tank x="0.8" y="0.0" z="-1.2" capacity="2990" jet="true"/>
<gear x="8.014" y="0.00" z="-2.2" compression="0.2" spring="0.2">
<control-input axis="/controls/gear/steering" control="STEER" invert="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="5"/>
</gear>
<gear x="-1.5" y="1.7" z="-2.55" compression=".5" spring="0.5">
<control-input axis="/controls/gear/brake-left" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/emer-brake" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="5"/>
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
</gear>
<gear x="-1.5" y="-1.7" z="-2.55" compression=".5" spring="0.5">
<control-input axis="/controls/gear/brake-right" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/emer-brake" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="5"/>
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
</gear>
<!--
Rolls Royce AE3007C1
40000 ft - thrust=1532 tsfc=0.650
Thrust Fuel flow(TSFC) 0.3222 kg/s, 0.3187 kg/s with winglets
-->
<jet x="-2.5" y="1.5" z="0.72" mass="1700" thrust="7000"
tsfc="0.3187" epr="23" rotate="0.0" egt="840" spool-time="2"
n1-idle="40" n1-max="103.8" n2-idle="56" n2-max="104.3">
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/reverser" control="REVERSE_THRUST"/>
<!-- <control-output control="REVERSE_THRUST" prop="surface-positions/reverser-norm"/> -->
<control-speed control="REVERSE_THRUST" transition-time="1.5"/>
<actionpt x="-5.0" y="1.5" z="0.72"/>
</jet>
<jet x="-2.5" y="-1.5" z="0.72" mass="1700" thrust="7000"
tsfc="0.3187" epr="23" rotate="0.0" egt="840" spool-time="2"
n1-idle="40" n1-max="103.8" n2-idle="56" n2-max="104.3">
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST"/>
<!-- <control-output control="REVERSE_THRUST" prop="surface-positions/reverser-norm[1]"/> -->
<control-speed control="REVERSE_THRUST" transition-time="1.5"/>
<actionpt x="-5.0" y="-1.5" z="0.72"/>
</jet>
<thruster x="0" y="0.00" z="0" vx="1" vy="0" vz="0" thrust="0">
<control-input axis="engines/engine/fan" control="THROTTLE"
src0="0" src1="40" dst0="0" dst1="1"/>
<control-output control="THROTTLE" prop="systems/hydraulics/psi-norm[0]"/>
<control-speed control="THROTTLE" transition-time="5"/>
</thruster>
<thruster x="0" y="0.00" z="0" vx="1" vy="0" vz="0" thrust="0">
<control-input axis="engines/engine[1]/fan" control="THROTTLE"
src0="0" src1="40" dst0="0" dst1="1"/>
<control-output control="THROTTLE" prop="systems/hydraulics/psi-norm[1]"/>
<control-speed control="THROTTLE" transition-time="5"/>
</thruster>
<ballast x="-6.0" y="0.0" z="2.0" mass="-1000"/>
<ballast x="-8.562" y="0" z="2.98" mass="-800"/>
<ballast x="0.0" y="0" z="-0.5" mass="5000"/>
<ballast x="-2.5" y="0" z="-0.5" mass="7000"/>
<ballast x="2.0" y="0" z="-0.5" mass="3000"/>
<weight x="7.0" y="0.0" z="0" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="-0.7" y="0" z="0" mass-prop="/sim/weight[1]/weight-lb"/>
<weight x="-1.5" y="0" z="0" mass-prop="/sim/weight[2]/weight-lb"/>
</airplane>