105 lines
4.2 KiB
XML
105 lines
4.2 KiB
XML
|
<airplane mass="16865">
|
||
|
|
|
||
|
|
<approach speed="58" aoa="13">
|
||
|
|
<control axis="/controls/throttle[0]" value="0.4"/>
|
||
|
|
<control axis="/controls/throttle[1]" value="0.4"/>
|
||
|
|
<control axis="/controls/mixture[0]" value="1.0"/>
|
||
|
|
<control axis="/controls/mixture[1]" value="1.0"/>
|
||
|
|
<control axis="/controls/propeller-pitch[0]" value="0.5"/>
|
||
|
|
<control axis="/controls/propeller-pitch[1]" value="0.5"/>
|
||
|
|
<control axis="/controls/flaps" value="1.0"/>
|
||
|
|
</approach>
|
||
|
|
<cruise speed="180" alt="23200">
|
||
|
|
<control axis="/controls/throttle[0]" value="1.0"/>
|
||
|
|
<control axis="/controls/throttle[1]" value="1.0"/>
|
||
|
|
<control axis="/controls/mixture[0]" value="1.0"/>
|
||
|
|
<control axis="/controls/mixture[1]" value="1.0"/>
|
||
|
|
<control axis="/controls/propeller-pitch[0]" value="1.0"/>
|
||
|
|
<control axis="/controls/propeller-pitch[1]" value="1.0"/>
|
||
|
|
<control axis="/controls/boost[0]" value="1.0"/>
|
||
|
|
<control axis="/controls/boost[1]" value="1.0"/>
|
||
|
|
<control axis="/controls/flaps" value="0.0"/>
|
||
|
|
</cruise>
|
||
|
|
|
||
|
|
<cockpit x="-1.63" y="0.41" z="0.76"/>
|
||
|
|
|
||
|
|
<fuselage ax="0" ay="0" az="0" bx="-19.75" by="0" bz="0"
|
||
|
|
width="2" taper="0.5" midpoint="0.25"/>
|
||
|
|
|
||
|
|
<wing x="-7.02" y="1.09" z="0.95" length="11.58" camber="0.1"
|
||
|
|
chord="4.77" taper=".286" sweep="19" dihedral="4">
|
||
|
|
<stall aoa="14" width="3" peak="1.5"/>
|
||
|
|
<flap0 start="0.04" end="0.38" lift="1.5" drag="2.0"/>
|
||
|
|
<flap1 start="0.38" end="0.97" lift="1.2" drag="1.5"/>
|
||
|
|
<control axis="/controls/flaps" output="FLAP0"/>
|
||
|
|
<control axis="/controls/aileron" output="FLAP1" split="true"/>
|
||
|
|
<control axis="/controls/aileron-trim" output="FLAP1" split="true"/>
|
||
|
|
</wing>
|
||
|
|
|
||
|
|
<hstab x="-18.12" y="0.41" z="0.27" length="3"
|
||
|
|
chord="3" taper=".545" sweep="15">
|
||
|
|
<stall aoa="14" width="3" peak="1.5"/>
|
||
|
|
<flap0 start="0" end="1" lift="1.5" drag="2.0"/>
|
||
|
|
<control axis="/controls/elevator" output="FLAP0"/>
|
||
|
|
<control axis="/controls/elevator-trim" output="FLAP0"/>
|
||
|
|
</hstab>
|
||
|
|
|
||
|
|
<vstab x="-18.12" y="0" z="0.95" length="2.72"
|
||
|
|
chord="3.95" taper=".462" sweep="2">
|
||
|
|
<stall aoa="14" width="3" peak="1.5"/>
|
||
|
|
<flap0 start="0" end="1" lift="1.5" drag="2.0"/>
|
||
|
|
<control axis="/controls/rudder" output="FLAP0" invert="true"/>
|
||
|
|
<control axis="/controls/rudder-trim" output="FLAP0" invert="true"/>
|
||
|
|
</vstab>
|
||
|
|
|
||
|
|
<propeller x="-4.09" y="2.52" z="-0.95"
|
||
|
|
mass="2000" moment="35" radius="1.4"
|
||
|
|
eng-power="1200" eng-rpm="2700"
|
||
|
|
turbo-mul="1.5"
|
||
|
|
cruise-power="660" cruise-speed="195"
|
||
|
|
cruise-rpm="2100" cruise-alt="20000"
|
||
|
|
min-rpm="1600" max-rpm="2700">
|
||
|
|
<actionpt x="-2.45" y="2.52" z="-0.95"/>
|
||
|
|
<control axis="/controls/throttle[0]" output="THROTTLE"/>
|
||
|
|
<control axis="/controls/mixture[0]" output="MIXTURE"/>
|
||
|
|
<control axis="/controls/propeller-pitch[0]" output="ADVANCE"/>
|
||
|
|
<control axis="/controls/boost[0]" output="BOOST"/>
|
||
|
|
</propeller>
|
||
|
|
|
||
|
|
<propeller x="-4.09" y="-2.52" z="-0.95"
|
||
|
|
mass="2000" moment="-35" radius="1.4"
|
||
|
|
eng-power="1200" eng-rpm="2700"
|
||
|
|
turbo-mul="1.5"
|
||
|
|
cruise-power="660" cruise-speed="195"
|
||
|
|
cruise-rpm="2100" cruise-alt="20000"
|
||
|
|
min-rpm="1600" max-rpm="2700">
|
||
|
|
<actionpt x="-2.45" y="-2.52" z="-0.95"/>
|
||
|
|
<control axis="/controls/throttle[1]" output="THROTTLE"/>
|
||
|
|
<control axis="/controls/mixture[1]" output="MIXTURE"/>
|
||
|
|
<control axis="/controls/propeller-pitch[1]" output="ADVANCE"/>
|
||
|
|
<control axis="/controls/boost[1]" output="BOOST"/>
|
||
|
|
</propeller>
|
||
|
|
|
||
|
|
<!-- Tail wheel; freely castering and uncontrollable -->
|
||
|
|
<gear x="-17.3" y="0" z="-1.5" compression="0.2" castering="true"/>
|
||
|
|
|
||
|
|
<!-- Main wheels; note mapping of rudder input to effect differential
|
||
|
|
braking -->
|
||
|
|
<gear x="-6.08" y="2.52" z="-3.49" compression="1" retract-time="7">
|
||
|
|
<control axis="/controls/brakes[0]" output="BRAKE"/>
|
||
|
|
<control axis="/controls/rudder" output="BRAKE"
|
||
|
|
src0="-1" src1="-0.5" dst0="1" dst1="0"/>
|
||
|
|
</gear>
|
||
|
|
|
||
|
|
<gear x="-6.08" y="-2.52" z="-3.49" compression="1" retract-time="7">
|
||
|
|
<control axis="/controls/brakes[1]" output="BRAKE"/>
|
||
|
|
<control axis="/controls/rudder" output="BRAKE"
|
||
|
|
src0="0.5" src1="1.0" dst0="0" dst1="1"/>
|
||
|
|
</gear>
|
||
|
|
|
||
|
|
<!-- From the type certificate: "Fuel capacity: 822 gals. (4 tanks in
|
||
|
|
center section wing: 2 main including fuel system 210 gals. each
|
||
|
|
(+48) and 2 aux. 201 gals. each (+83.5)" -->
|
||
|
|
<tank x="-7.02" y="0" z="0.95" capacity="4932"/>
|
||
|
|
|
||
|
|
</airplane>
|