105 lines
No EOL
4.2 KiB
XML
105 lines
No EOL
4.2 KiB
XML
<airplane mass="16865">
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<approach speed="58" aoa="13">
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<control axis="/controls/throttle[0]" value="0.4"/>
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<control axis="/controls/throttle[1]" value="0.4"/>
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<control axis="/controls/mixture[0]" value="1.0"/>
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<control axis="/controls/mixture[1]" value="1.0"/>
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<control axis="/controls/propeller-pitch[0]" value="0.5"/>
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<control axis="/controls/propeller-pitch[1]" value="0.5"/>
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<control axis="/controls/flaps" value="1.0"/>
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</approach>
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<cruise speed="180" alt="23200">
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<control axis="/controls/throttle[0]" value="1.0"/>
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<control axis="/controls/throttle[1]" value="1.0"/>
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<control axis="/controls/mixture[0]" value="1.0"/>
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<control axis="/controls/mixture[1]" value="1.0"/>
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<control axis="/controls/propeller-pitch[0]" value="1.0"/>
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<control axis="/controls/propeller-pitch[1]" value="1.0"/>
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<control axis="/controls/boost[0]" value="1.0"/>
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<control axis="/controls/boost[1]" value="1.0"/>
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<control axis="/controls/flaps" value="0.0"/>
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</cruise>
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<cockpit x="-1.63" y="0.41" z="0.76"/>
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<fuselage ax="0" ay="0" az="0" bx="-19.75" by="0" bz="0"
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width="2" taper="0.5" midpoint="0.25"/>
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<wing x="-7.02" y="1.09" z="0.95" length="11.58" camber="0.1"
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chord="4.77" taper=".286" sweep="19" dihedral="4">
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<stall aoa="14" width="3" peak="1.5"/>
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<flap0 start="0.04" end="0.38" lift="1.5" drag="2.0"/>
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<flap1 start="0.38" end="0.97" lift="1.2" drag="1.5"/>
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<control axis="/controls/flaps" output="FLAP0"/>
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<control axis="/controls/aileron" output="FLAP1" split="true"/>
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<control axis="/controls/aileron-trim" output="FLAP1" split="true"/>
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</wing>
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<hstab x="-18.12" y="0.41" z="0.27" length="3"
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chord="3" taper=".545" sweep="15">
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<stall aoa="14" width="3" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.5" drag="2.0"/>
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<control axis="/controls/elevator" output="FLAP0"/>
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<control axis="/controls/elevator-trim" output="FLAP0"/>
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</hstab>
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<vstab x="-18.12" y="0" z="0.95" length="2.72"
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chord="3.95" taper=".462" sweep="2">
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<stall aoa="14" width="3" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.5" drag="2.0"/>
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<control axis="/controls/rudder" output="FLAP0" invert="true"/>
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<control axis="/controls/rudder-trim" output="FLAP0" invert="true"/>
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</vstab>
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<propeller x="-4.09" y="2.52" z="-0.95"
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mass="2000" moment="35" radius="1.4"
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eng-power="1200" eng-rpm="2700"
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turbo-mul="1.5"
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cruise-power="660" cruise-speed="195"
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cruise-rpm="2100" cruise-alt="20000"
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min-rpm="1600" max-rpm="2700">
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<actionpt x="-2.45" y="2.52" z="-0.95"/>
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<control axis="/controls/throttle[0]" output="THROTTLE"/>
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<control axis="/controls/mixture[0]" output="MIXTURE"/>
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<control axis="/controls/propeller-pitch[0]" output="ADVANCE"/>
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<control axis="/controls/boost[0]" output="BOOST"/>
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</propeller>
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<propeller x="-4.09" y="-2.52" z="-0.95"
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mass="2000" moment="-35" radius="1.4"
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eng-power="1200" eng-rpm="2700"
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turbo-mul="1.5"
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cruise-power="660" cruise-speed="195"
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cruise-rpm="2100" cruise-alt="20000"
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min-rpm="1600" max-rpm="2700">
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<actionpt x="-2.45" y="-2.52" z="-0.95"/>
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<control axis="/controls/throttle[1]" output="THROTTLE"/>
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<control axis="/controls/mixture[1]" output="MIXTURE"/>
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<control axis="/controls/propeller-pitch[1]" output="ADVANCE"/>
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<control axis="/controls/boost[1]" output="BOOST"/>
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</propeller>
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<!-- Tail wheel; freely castering and uncontrollable -->
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<gear x="-17.3" y="0" z="-1.5" compression="0.2" castering="true"/>
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<!-- Main wheels; note mapping of rudder input to effect differential
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braking -->
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<gear x="-6.08" y="2.52" z="-3.49" compression="1" retract-time="7">
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<control axis="/controls/brakes[0]" output="BRAKE"/>
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<control axis="/controls/rudder" output="BRAKE"
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src0="-1" src1="-0.5" dst0="1" dst1="0"/>
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</gear>
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<gear x="-6.08" y="-2.52" z="-3.49" compression="1" retract-time="7">
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<control axis="/controls/brakes[1]" output="BRAKE"/>
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<control axis="/controls/rudder" output="BRAKE"
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src0="0.5" src1="1.0" dst0="0" dst1="1"/>
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</gear>
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<!-- From the type certificate: "Fuel capacity: 822 gals. (4 tanks in
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center section wing: 2 main including fuel system 210 gals. each
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(+48) and 2 aux. 201 gals. each (+83.5)" -->
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<tank x="-7.02" y="0" z="0.95" capacity="4932"/>
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</airplane> |