78 lines
No EOL
2.8 KiB
XML
78 lines
No EOL
2.8 KiB
XML
<airplane mass="1950">
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<!-- Approach configuration -->
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<approach speed="40" aoa="16">
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<control axis="/controls/throttle[0]" value="0.3"/>
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<control axis="/controls/mixture[0]" value="1.0"/>
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<control axis="/controls/flaps" value="1.0"/>
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</approach>
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<!-- Cruise configuration -->
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<cruise speed="115" alt="8000">
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<control axis="/controls/throttle[0]" value="1.0"/>
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<control axis="/controls/mixture[0]" 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="-1.88" y=".33" z="0.6"/>
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<fuselage ax="-.17" ay="0" az="-.51" bx="-7.16" by="0" bz=".17" width="1"/>
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<!-- Extra fuselage to handle the "bulge" at the front -->
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<fuselage ax="-1.36" ay="0" az=".17" bx="-4.09" by="0" bz=".17" width="1"/>
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<wing x="-2.47" y=".51" z=".68" taper=".78"
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length="5.37" chord="1.54" sweep="0" dihedral="0" camber="0.1">
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<stall aoa="16" width="4" peak="1.5"/>
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<flap0 start="0" end=".38" lift="1.6" drag="2.0"/>
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<flap1 start=".78" end="1" lift="1.5" drag="1.6"/>
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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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</wing>
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<hstab x="-7.16" y="0.08" z=".17" taper=".63" effectiveness="2"
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length="1.71" chord="1.36" sweep="0">
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<stall aoa="16" width="4" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.6" drag="1.8"/>
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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="-7.16" y="0" z=".17" taper=".5" effectiveness="3"
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length="1.71" chord="1.54" sweep="20">
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<stall aoa="16" width="4" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.3" drag="1.5"/>
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<control axis="/controls/rudder" output="FLAP0" invert="true" square="true"/>
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</vstab>
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<propeller radius="1.0"
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cruise-speed="86" cruise-rpm="2200"
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cruise-alt="10000" cruise-power="99"
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takeoff-power="180" takeoff-rpm="2500"
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eng-power="180" eng-rpm="2500"
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x="-.6" y="0" z="0" mass="400" moment="11">
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<actionpt x="0" y="0" z="0"/>
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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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</propeller>
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<gear x="-1" y="0" z="-1.5" compression=".4"> <!-- nose -->
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<control axis="/controls/rudder" output="STEER"/>
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</gear>
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<gear x="-2.73" y="1.15" z="-1.36" compression=".3"> <!-- left main -->
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<control axis="/controls/brakes[0]" output="BRAKE"/>
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</gear>
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<gear x="-2.73" y="-1.15" z="-1.36" compression=".3"> <!-- left main -->
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<control axis="/controls/brakes[1]" output="BRAKE"/>
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</gear>
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<tank x="-2.47" y="1.36" z=".68" capacity="75"/>
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<tank x="-2.47" y="-1.36" z=".68" capacity="75"/>
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<ballast x="-2.0" y=".33" z="0" mass="180"/> <!-- pilot -->
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<ballast x="-2.0" y="-.33" z="0" mass="180"/> <!-- passenger -->
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<ballast x="-1.0" y="-.33" z="0" mass="200"/> <!-- cockpit -->
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</airplane> |