2002-12-12 18:55:58 +00:00
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<airplane mass="1480">
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<!-- Approach configuration -->
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2003-02-18 16:54:23 +00:00
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<approach speed="45" aoa="14">
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<control-setting axis="/controls/throttle[0]" value="0.0"/>
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2002-12-12 18:55:58 +00:00
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<control-setting axis="/controls/mixture[0]" value="1.0"/>
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2003-02-18 16:54:23 +00:00
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<control-setting axis="/controls/flaps" value="0.0"/>
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2002-12-12 18:55:58 +00:00
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</approach>
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<!-- Cruise configuration -->
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2003-02-18 16:54:23 +00:00
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<cruise speed="123" alt="7000">
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2002-12-12 18:55:58 +00:00
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<control-setting axis="/controls/throttle[0]" value="1.0"/>
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2003-02-18 16:54:23 +00:00
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<control-setting axis="/controls/mixture[0]" value="0.7"/>
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2002-12-12 18:55:58 +00:00
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<control-setting axis="/controls/flaps" value="0.0"/>
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</cruise>
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<cockpit x="-2.5" y=".33" z="0.6"/>
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<fuselage ax="0.5" ay="0" az="0" bx="-7.75" by="0" bz="0"
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width="1.5" taper="0.2" midpoint="0.3"/>
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2003-02-18 16:54:23 +00:00
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<wing x="-2.75" y="0.6" z="-0.75" taper="0.65" incidence="2" twist="-2"
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2002-12-12 18:55:58 +00:00
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length="4.5" chord="1.65" sweep="0" dihedral="5" camber="0.1">
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2003-02-18 16:54:23 +00:00
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<stall aoa="18" width="2.0" peak="1.5"/>
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2003-02-18 17:41:29 +00:00
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<flap0 start="0" end="0.5" lift="1.5" drag="1.5"/>
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2002-12-12 18:55:58 +00:00
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<flap1 start="0.5" end="1.0" lift="1.2" drag="1.2"/>
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<control-input axis="/controls/flaps" control="FLAP0"/>
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<control-input axis="/controls/aileron" control="FLAP1" split="true"/>
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<control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/>
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<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
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<control-output control="FLAP1" side="left"
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prop="/surface-positions/left-aileron-pos-norm"/>
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<control-output control="FLAP1" side="right"
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prop="/surface-positions/right-aileron-pos-norm"/>
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</wing>
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2003-02-18 16:54:23 +00:00
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<hstab x="-6.5" y="0.00" z=".15" taper="1.0" effectiveness="2" incidence="-1"
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2002-12-12 18:55:58 +00:00
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length="1.9" chord="0.9" sweep="0">
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2003-02-18 16:54:23 +00:00
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<stall aoa="17" width="4" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.65" drag="1.2"/>
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2002-12-12 18:55:58 +00:00
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<control-input axis="/controls/elevator" control="FLAP0"/>
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<control-input axis="/controls/elevator-trim" control="FLAP0"/>
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<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
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</hstab>
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<vstab x="-6.25" y="0" z=".3" taper=".5"
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length="1.2" chord="1.2" sweep="10">
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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="1.1"/>
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<control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
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<control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/>
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<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
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min="1" max="-1"/>
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</vstab>
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<propeller radius="1.0"
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cruise-speed="125" cruise-rpm="2665"
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cruise-alt="8000" cruise-power="120"
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takeoff-power="140.8" takeoff-rpm="2200"
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eng-power="160" eng-rpm="2800"
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x="-1" y="0" z="0" mass="400" moment="8">
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<actionpt x="0" y="0" z="0"/>
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<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
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<control-input axis="/controls/starter[0]" control="STARTER"/>
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<control-input axis="/controls/magnetos[0]" control="MAGNETOS"/>
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<control-input axis="/controls/mixture[0]" control="MIXTURE"/>
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</propeller>
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2002-12-18 02:03:46 +00:00
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<gear x="-1" y="0" z="-1.3" compression=".05"> <!-- nose -->
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2002-12-12 18:55:58 +00:00
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<control-input axis="/controls/rudder" control="STEER"
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src0="-1.0" src1="1.0"
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dst0="-0.1" dst1="0.1"/>
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</gear>
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2002-12-18 02:03:46 +00:00
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<gear x="-2.8" y="1.5" z="-1.3" compression=".05"> <!-- left main -->
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2002-12-12 18:55:58 +00:00
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<control-input axis="/controls/brakes[0]" control="BRAKE" split="true"/>
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<control-input axis="/controls/parking-brake" control="BRAKE" split="true"/>
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</gear>
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2002-12-18 02:03:46 +00:00
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<gear x="-2.8" y="-1.5" z="-1.3" compression=".05"> <!-- left main -->
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2002-12-12 18:55:58 +00:00
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<control-input axis="/controls/brakes[1]" control="BRAKE" split="true"/>
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<control-input axis="/controls/parking-brake" control="BRAKE" split="true"/>
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</gear>
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<tank x="-2.5" y="1.5" z="-0.25" capacity="144"/>
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<tank x="-2.5" y="-1.5" z="-0.25" capacity="144"/>
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2002-12-18 02:03:46 +00:00
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<ballast x="-2.0" y="0" z="0" mass="400"/> <!-- cockpit -->
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2002-12-12 18:55:58 +00:00
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<weight x="-2.5" y=".33" z="0" mass-prop="/yasim/pa28/pilot-lb"/>
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<weight x="-2.5" y="-.33" z="0" mass-prop="/yasim/pa28/copilot-lb"/>
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</airplane>
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