/
dhc6.xml
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dhc6.xml
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<?xml version="1.0" encoding="UTF-8"?>
<!--
DHC6-300 Twin Otter
Jan 2008 by Syd Adams.
SPECS:
Height: 5.9m
Length: 15.77
Wing span: 19.8
MTOW: 12,500 lbs
Service Ceiling = 26700 ft
Cruise at MTOW
5000 ft - 181 TAS
10,000 ft - 182 TAS
Stall :
Full Flaps = 58 kt
O Flaps = 74 kt
-->
<airplane mass="7500">
<approach speed="73" aoa="6.0" fuel="0.5">
<control-setting axis="/controls/engines/engine[0]/internal-throttle-fwd" value="0.30"/>
<control-setting axis="/controls/engines/engine[1]/internal-throttle-fwd" value="0.30"/>
<control-setting axis="/controls/engines/engine[0]/internal-condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/internal-condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/propeller-pitch" value="1.0"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="3150"/>
</approach>
<cruise speed="176" alt="10000" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/internal-throttle-fwd" value="1"/>
<control-setting axis="/controls/engines/engine[1]/internal-throttle-fwd" value="1"/>
<control-setting axis="/controls/engines/engine[0]/internal-condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/internal-condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="0.96"/>
<control-setting axis="/controls/engines/engine[1]/propeller-pitch" value="0.96"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="3350"/>
</cruise>
<cockpit x="2.8" y="0.3" z="0.745"/>
<fuselage ax="6.338" ay="0" az="-0.185" bx="3.609" by="0" bz="0.111"
width="1.8" taper="0.2" midpoint="1.0" cy="1.1" cx="1.1"/>
<fuselage ax="3.609" ay="0" az="0.111" bx="-2.470" by="0" bz="0.111"
width="1.8" taper="1.0" midpoint="0.5" cy="1.1" cx="1.1" />
<fuselage ax="-2.470" ay="0" az="0.111" bx="-8.811" by="0" bz="0.30"
width="1.8" taper="0.1" midpoint="0.0" cy="1.1" cx="1.1" />
<fuselage ax="2.497" ay="2.857" az="0.858" bx="-0.410" by="2.857" bz="1.012"
width="0.6" taper="0.2" midpoint="0.2" cy="1.5" cx="1.5" />
<fuselage ax="2.497" ay="-2.857" az="0.858" bx="-0.410" by="-2.857" bz="1.012"
width="0.6" taper="0.2" midpoint="0.2" cy="1.5" cx="1.5" />
<wing x="0.0" y="0.80" z="1.0" length="9.0" chord="2.0"
sweep="0" dihedral="3" taper="1" incidence="2.5" idrag="1.0" camber="0.24">
<stall aoa="10" width="6" peak="1.5"/>
<flap0 start="0" end="0.90" lift="1.6" drag="3.2"/>
<flap1 start="0.6" end="0.90" lift="1.2" drag="1.2"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-speed control="FLAP0" transition-time="20"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<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"/>
</wing>
<hstab x="-7.47" y="0.08" z="1.186" length="3.15" chord="1.4"
sweep="0" dihedral="0" taper="1" camber="-0.05">
<stall aoa="17" width="6" peak="1.5"/>
<flap0 start="0" end="1" lift="1.7" drag="1.5"/>
<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="-7.312" y="0.00" z="0.3" length="2.6" chord="2.9"
sweep="20" taper="0.7" >
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
<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"/>
</vstab>
<!-- frt doors-->
<vstab x="0" y="0" z="0" length="0.001" chord="0.001">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="0.5" lift="0" drag="0"/>
<control-input axis="/controls/doors/LF-door/open" control="FLAP0"/>
<control-output control="FLAP0" prop="/controls/doors/LF-door/position-norm"/>
<control-speed control="FLAP0" transition-time="2"/>
<control-input axis="/controls/doors/RF-door/open" control="FLAP1"/>
<control-output control="FLAP1" prop="/controls/doors/RF-door/position-norm"/>
<control-speed control="FLAP1" transition-time="2"/>
</vstab>
<!-- rear doors pasenger-->
<vstab x="0" y="0" z="0" length="0.001" chord="0.001">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="0.5" lift="0" drag="0"/>
<control-input axis="/controls/doors/LR-door-F/open" control="FLAP0"/>
<control-output control="FLAP0" prop="/controls/doors/LR-door-F/position-norm"/>
<control-speed control="FLAP0" transition-time="2"/>
<control-input axis="/controls/doors/RR-door/open" control="FLAP1"/>
<control-output control="FLAP1" prop="/controls/doors/RR-door/position-norm"/>
<control-speed control="FLAP1" transition-time="2"/>
</vstab>
<!-- rear door baggage -->
<vstab x="0" y="0" z="0" length="0.001" chord="0.001">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="0.5" lift="0" drag="0"/>
<control-input axis="/controls/doors/LR-door-R/open" control="FLAP0"/>
<control-output control="FLAP0" prop="/controls/doors/LR-door-R/position-norm"/>
<control-speed control="FLAP0" transition-time="2"/>
<control-input axis="/controls/doors/Baggage.door/open" control="FLAP1"/>
<control-output control="FLAP1" prop="/controls/doors/Baggage.door/position-norm"/>
<control-speed control="FLAP1" transition-time="2"/>
</vstab>
<!--
2500 lbs (Jet A)
Fuel burn ... 580 lbs/hr
-->
<tank x="0.66" y="0" z="-0.5" capacity="1000" jet="true"/>
<tank x="-1.32" y="0" z="0.5" capacity="1400" jet="true"/>
<tank x="0" y="0" z="0" capacity="0"/>
<gear x="4.468" y="0.00" z="-1.782" compression=".3"
spring="1.2" damp="1.0" sfric="1.4" dfric="0.7">
<control-input axis="/controls/gear/tiller" control="STEER" square="true"/>
</gear>
<gear x="-1" y="2.65" z="-1.83" compression=".3"
spring="1.0" damp="0.6" sfric="1.4" dfric="1.2">
<control-input axis="/controls/gear/brake-left" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
</gear>
<gear x="-1" y="-2.65" z="-1.83" compression=".3"
spring="1.0" damp="0.6" sfric="1.4" dfric="1.2">
<control-input axis="/controls/gear/brake-right" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
</gear>
<!--
Engines:
2 PT6A-27
620 shp
Prop diam: 2.59 m
-->
<propeller x="1.3" y="2.65" z="1.0"
mass="500" moment="40" radius="1.1"
cruise-speed="146" cruise-rpm="1650"
cruise-power="484" cruise-alt="10000"
min-rpm="1650" max-rpm="2110"
fine-stop="0.2" coarse-stop="4.0">
<turbine-engine
eng-power="620" eng-rpm="2110" alt="0"
flat-rating="620" n2-low-idle="50" n2-high-idle="50" n2-max="101.5" bsfc="0.6"/>
<actionpt x="2.2" y="2.65" z="1.0"/>
<control-input axis="/controls/engines/engine[0]/internal-throttle-fwd"
src0="0" dst0="0.05" src1="1" dst1="1" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/internal-condition"
control="CONDLEVER"/>
<control-input axis="/controls/engines/engine[0]/starter"
control="STARTER"/>
<control-input axis="/controls/engines/engine[0]/propeller-pitch"
control="ADVANCE"/>
<control-input axis="/controls/engines/engine[0]/propeller-feather"
control="PROPFEATHER"/>
</propeller>
<propeller x="1.3" y="-2.65" z="1.1"
mass="500" moment="40" radius="1.0"
cruise-speed="146" cruise-rpm="1650"
cruise-power="484" cruise-alt="10000"
min-rpm="1650" max-rpm="2110"
fine-stop="0.2" coarse-stop="4.0">
<turbine-engine
eng-power="620" eng-rpm="2110" alt="0"
flat-rating="620" n2-low-idle="50" n2-high-idle="50" n2-max="101.5" bsfc="0.6"/>
<actionpt x="2.2" y="-2.65" z="1.0"/>
<control-input axis="/controls/engines/engine[1]/internal-throttle-fwd"
src0="0" dst0="0.05" src1="1" dst1="1" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/internal-condition"
control="CONDLEVER"/>
<control-input axis="/controls/engines/engine[1]/starter"
control="STARTER"/>
<control-input axis="/controls/engines/engine[1]/propeller-pitch"
control="ADVANCE"/>
<control-input axis="/controls/engines/engine[1]/propeller-feather"
control="PROPFEATHER"/>
</propeller>
<thruster x="2.2" y="2.65" z="1.0" vx="-1" vy="0" vz="0" thrust="1600">
<control-input axis="/controls/engines/engine[0]/internal-throttle-rvrs" control="THROTTLE"/>
<control-output control="THROTTLE" prop="engines/engine[0]/reverse"/>
<control-speed control="THROTTLE" transition-time="2"/>
</thruster>
<thruster x="2.2" y="-2.65" z="1.0" vx="-1" vy="0" vz="0" thrust="1600">
<control-input axis="/controls/engines/engine[1]/internal-throttle-rvrs" control="THROTTLE"/>
<control-output control="THROTTLE" prop="engines/engine[1]/reverse"/>
<control-speed control="THROTTLE" transition-time="2"/>
</thruster>
<weight x="2.5" y="0" z="0" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="0.0" y="0" z="0" mass-prop="/sim/weight[1]/weight-lb"/>
<ballast x="5" y="0" z="-2.5" mass="2078"/>
<hitch name="aerotow" x="-2.5" y="0" z="-0.85" force-is-calculated-by-other="1">
<tow length="60" weight-per-meter="0.035" elastic-constant="9000" break-force="10000" mp-auto-connect-period="1.0"/>
<winch max-tow-length="1000" min-tow-length="60" initial-tow-length="60"/>
</hitch>
</airplane>