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L-188F.xml
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L-188F.xml
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<!--
wingspan 35.8 m
length
wing area 135.9 m2
approach (full flap) 115 kt
landing speed (full flap) 107 kt
400 gph/2200 rpm max cruise speed
dirty stall 81 kts @ MLW ( 88,000 lbs)
MTOW 107000 lbs
-->
<airplane mass="55357">
<approach speed="110" aoa="6" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.25"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.25"/>
<control-setting axis="/controls/engines/engine[2]/throttle" value="0.25"/>
<control-setting axis="/controls/engines/engine[3]/throttle" value="0.25"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/mixture" value="1.0"/>
<control-setting axis="/controls/engines/engine[2]/mixture" value="1.0"/>
<control-setting axis="/controls/engines/engine[3]/mixture" value="1.0"/>
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="1"/>
<control-setting axis="/controls/engines/engine[1]/propeller-pitch" value="1"/>
<control-setting axis="/controls/engines/engine[2]/propeller-pitch" value="1"/>
<control-setting axis="/controls/engines/engine[3]/propeller-pitch" value="1"/>
<control-setting axis="/controls/flight/flaps" value="1"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<solve-weight idx="0" weight="500"/>
<solve-weight idx="1" weight="15000"/>
</approach>
<cruise speed="390" alt="20000" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/throttle" value="1"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="1"/>
<control-setting axis="/controls/engines/engine[2]/throttle" value="1"/>
<control-setting axis="/controls/engines/engine[3]/throttle" value="1"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="1"/>
<control-setting axis="/controls/engines/engine[1]/mixture" value="1"/>
<control-setting axis="/controls/engines/engine[2]/mixture" value="1"/>
<control-setting axis="/controls/engines/engine[3]/mixture" value="1"/>
<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/engines/engine[2]/propeller-pitch" value="1.0"/>
<control-setting axis="/controls/engines/engine[3]/propeller-pitch" value="1.0"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<solve-weight idx="0" weight="500"/>
<solve-weight idx="1" weight="15000"/>
</cruise>
<cockpit x="9.182" y="0.56" z="1.32"/>
<fuselage ax="12.125" ay="0" az="0.177" bx="7.57" by="0" bz="0.693"
width="3" taper="0.5" midpoint="1.0"/>
<fuselage ax="7.57" ay="0" az="0.693" bx="-7.57" by="0" bz="0.693"
width="3" taper="1"/>
<fuselage ax="-7.57" ay="0" az="0.693" bx="-14.0" by="0" bz="0.693"
width="3" taper="0.8" midpoint="0"/>
<fuselage ax="-14.0" ay="0" az="0.693" bx="-19.62" by="0" bz="0.693"
width="3" taper="0" midpoint="0"/>
<fuselage ax="5" ay="0" az="-0.164" bx="-5" by="0" bz="-0.164"
width="2" taper="1" midpoint="0.5"/>
<!-- engines -->
<fuselage ax="-5.03" ay="-8.08" az="0.265" bx="1.07" by="-8.08" bz="0.265"
width="1.6" taper="0.3" midpoint="0.33"/>
<fuselage ax="-5.03" ay="8.08" az="0.265" bx="1.07" by="8.08" bz="0.265"
width="1.6" taper="0.3" midpoint="0.33"/>
<fuselage ax="-5.89" ay="-3.855" az="-0.086" bx="0.204" by="-3.855" bz="-0.086"
width="1.6" taper="0.3" midpoint="0.33"/>
<fuselage ax="-5.89" ay="3.855" az="-0.086" bx="0.204" by="3.855" bz="-0.086"
width="1.6" taper="0.3" midpoint="0.33"/>
<wing x="-0.37" y="1.50" z="-0.5" length="16.4" camber="0.02"
chord="5.60" taper=".4797" sweep="1" dihedral="7">
<stall aoa="15" width="7" peak="1.5"/>
<flap0 start="0.04" end="0.38" lift="1.5" drag="1.7"/>
<flap1 start="0.38" end="0.97" lift="1.2" drag="1.2"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<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"/>
<control-speed control="FLAP0" transition-time="5"/>
</wing>
<hstab x="-16.77" y="1.23" z="0.621" length="6.03"
chord="3.16" taper=".4" sweep="0" incidence="0" camber="-0.08">
<stall aoa="15" width="3" peak="1.5"/>
<flap0 start="0" end="1" lift="1.6" drag="1.2"/>
<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="-16.33" y="0" z="1.75 " length="4.5"
chord="4.67" taper=".5" sweep="10">
<stall aoa="14" width="3" peak="1.5"/>
<flap0 start="0" end="1" lift="1.6" 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>
<!-- Pratt & Whitney R-2800 Double Wasp -->
<propeller x="2.881" y="8.08" z="0.265" moment="90" mass="2600"
radius="1.98" cruise-power="2000" cruise-alt="20000"
min-rpm="1400" max-rpm="2800" cruise-speed="390" cruise-rpm="2200"
fine-stop="0.25" coarse-stop="4">
<piston-engine eng-rpm="2800" eng-power="2500"
displacement="2804" compression="6.75"
turbo-mul="2.5" wastegate-mp="60" turbo-lag="0.2"/>
<actionpt x="4.46" y="8.08" z="0.265"/>
<control-input control="THROTTLE" axis="/controls/engines/engine[0]/throttle"/>
<control-input control="STARTER" axis="/controls/engines/engine[0]/starter"/>
<control-input control="MAGNETOS" axis="/controls/engines/engine[0]/magnetos"/>
<control-input control="MIXTURE" axis="/controls/engines/engine[0]/mixture"/>
<control-input control="ADVANCE" axis="/controls/engines/engine[0]/propeller-pitch"/>
</propeller>
<propeller x="3.746" y="3.855" z="-0.08" moment="90" mass="2600"
radius="1.98" cruise-power="2000" cruise-alt="20000"
min-rpm="1400" max-rpm="2800" cruise-speed="390" cruise-rpm="2200"
fine-stop="0.25" coarse-stop="4">
<piston-engine eng-rpm="2800" eng-power="2500"
displacement="2804" compression="6.75"
turbo-mul="2.5" wastegate-mp="60" turbo-lag="0.2"/>
<actionpt x="5.325" y="3.855" z="-0.08"/>
<control-input control="THROTTLE" axis="/controls/engines/engine[1]/throttle"/>
<control-input control="STARTER" axis="/controls/engines/engine[1]/starter"/>
<control-input control="MAGNETOS" axis="/controls/engines/engine[1]/magnetos"/>
<control-input control="MIXTURE" axis="/controls/engines/engine[1]/mixture"/>
<control-input control="ADVANCE" axis="/controls/engines/engine[1]/propeller-pitch"/>
</propeller>
<propeller x="3.746" y="-3.855" z="-0.08" moment="90" mass="2600"
radius="1.98" cruise-power="2000" cruise-alt="20000"
min-rpm="1400" max-rpm="2800" cruise-speed="390" cruise-rpm="2200"
fine-stop="0.25" coarse-stop="4">
<piston-engine eng-rpm="2800" eng-power="2500"
displacement="2804" compression="6.75"
turbo-mul="2.5" wastegate-mp="60" turbo-lag="0.2"/>
<actionpt x="5.325" y="-3.855" z="-0.08"/>
<control-input control="THROTTLE" axis="/controls/engines/engine[2]/throttle"/>
<control-input control="STARTER" axis="/controls/engines/engine[2]/starter"/>
<control-input control="MAGNETOS" axis="/controls/engines/engine[2]/magnetos"/>
<control-input control="MIXTURE" axis="/controls/engines/engine[2]/mixture"/>
<control-input control="ADVANCE" axis="/controls/engines/engine[2]/propeller-pitch"/>
</propeller>
<propeller x="2.881" y="-8.08" z="0.265" moment="90" mass="2600"
radius="1.98" cruise-power="2000" cruise-alt="20000"
min-rpm="1400" max-rpm="2800" cruise-speed="390" cruise-rpm="2200"
fine-stop="0.25" coarse-stop="4">
<piston-engine eng-rpm="2800" eng-power="2500"
displacement="2804" compression="6.75"
turbo-mul="2.5" wastegate-mp="60" turbo-lag="0.2"/>
<actionpt x="4.46" y="-8.08" z="0.265"/>
<control-input control="THROTTLE" axis="/controls/engines/engine[3]/throttle"/>
<control-input control="STARTER" axis="/controls/engines/engine[3]/starter"/>
<control-input control="MAGNETOS" axis="/controls/engines/engine[3]/magnetos"/>
<control-input control="MIXTURE" axis="/controls/engines/engine[3]/mixture"/>
<control-input control="ADVANCE" axis="/controls/engines/engine[3]/propeller-pitch"/>
</propeller>
<gear x="8.83209" y="0" z="-3.083" compression="0.3">
<control-input axis="/controls/flight/rudder" control="STEER" square="true" src0="-1" src1="1.75" dst0="-1" dst1="1.75"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="5"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
<control-output control="STEER" prop="/gear/gear[0]/steering-norm"/>
</gear>
<gear x="-2.58126" y="4.75116" z="-2.96" compression="0.3" retract-time="7"
spring="1" damp="10">
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/brake-left" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="5"/>
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
</gear>
<gear x="-2.58126" y="-4.75116" z="-2.96" compression="0.3" retract-time="7"
spring="1" damp="10">
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/brake-right" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="5"/>
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
</gear>
<tank x="0.2" y="12.0" z="0.75" capacity="4170"/><!-- Outer Main #1-->
<tank x="0.275" y="8.15" z="0.287" capacity="4314"/><!-- Inner Main #2-->
<tank x="0.327" y="5.5" z="-0.03" capacity="3480"/><!-- Outer Alt #1 -->
<tank x="0.388" y="2.33" z="-0.413" capacity="4572"/><!-- Inner Alt #2-->
<tank x="0.388" y="-2.33" z="-0.413" capacity="4572"/><!-- Inner Alt #3-->
<tank x="0.327" y="-5.5" z="-0.03" capacity="3480"/><!-- Outer Alt #4-->
<tank x="0.275" y="-8.15" z="0.287" capacity="4314"/><!-- Inner Main #3-->
<tank x="0.2" y="-12.0" z="0.75" capacity="4170"/><!-- Outer Main #4-->
<tank x="0" y="0" z="0" capacity="0"/><!-- Dummy-->
<ballast x="-16.0" y="0.0" z="1" mass="-6500"/>
<ballast x="0.0" y="0.0" z="-1.5" mass="15000"/>
<weight x="9.0" y="0.0" z="0.0" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="0.5" y="0.0" z="0.0" mass-prop="/sim/weight[1]/weight-lb"/>
<thruster x="19.28" y="0.00" z="-5.55" vx="1" vy="0" vz="0" thrust="20000">
<control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE"
src0="-1" src1="1" dst0="-1.5" dst1="1.5"/>
</thruster>
</airplane>