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Revert previous update

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jimw 2003-05-07 01:52:04 +00:00
parent bdcfe0c357
commit 10c6842beb
1 changed files with 153 additions and 154 deletions
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21
Aircraft-yasim/p51d.xml
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@ -32,8 +32,8 @@ The reference datum for measurements is the nose.
<airplane mass="7390">
<!-- Approach configuration -->
<approach speed="87" aoa="13">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
<approach speed="150" aoa="6.6">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="0.5"/>
<control-setting axis="/controls/flight/flaps" value="1.0"/>
@ -61,8 +61,8 @@ The reference datum for measurements is the nose.
stall aoa not available
flap drag not available
-->
<wing x="-3.96" y="0.49" z="-0.67" taper="0.466" incidence="-1"
length="5.16" chord="2.845" sweep="3.5" dihedral="5" camber=".1">
<wing x="-3.96" y="0.49" z="-0.67" taper="0.466" incidence="1"
length="5.16" chord="2.845" sweep="3.5" dihedral="5">
<stall aoa="14" width="4" peak="1.5"/>
<flap0 start="0.024" end="0.543" lift="1.2" drag="1.4"/>
<flap1 start="0.543" end="0.97" lift="1.2" drag="1.4"/>
@ -73,17 +73,17 @@ flap drag not available
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
</wing>
<hstab x="-8.62" y="0.18" z="0.35" taper="0.639" effectiveness="4.0"
<hstab x="-8.62" y="0.18" z="0.35" taper="0.639" effectiveness="1.0"
length="1.834" chord="1.256" sweep="0" incidence="2">
<stall aoa="15" width="4" peak="1.5"/>
<flap0 start="0.0" end="1.8" lift="1.65" drag="1.2"/>
<flap0 start="0.0" end="1.8" lift="1.5" 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>
<!-- rudder has to be able to counteract aileron drag -->
<vstab x="-9.30" y="0" z="-0.37" taper="0.432" effectiveness="4.0"
<vstab x="-9.30" y="0" z="-0.37" taper="0.432" effectiveness="1.5"
length="1.971" chord="2.65" sweep="25">
<stall aoa="15" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.3" drag="1.2"/>
@ -110,12 +110,11 @@ flap drag not available
<control-input axis="/controls/engines/engine[0]/boost" control="BOOST"/>
</propeller>
<!-- Tail wheel -->
<gear x="-7.90" y="0" z="-1.03" compression="0.2">
<gear x="-7.90" y="0" z="-1.03" compression="0.8" spring="1.0" damp="2">
</gear>
<!-- left main -->
<gear x="-2.79" y="1.81" z="-2.20" compression="0.8" spring="1.0">
<gear x="-2.79" y="1.81" z="-2.20" compression="0.8" spring="1.0" damp="3">
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
<control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
@ -124,7 +123,7 @@ flap drag not available
</gear>
<!-- right main -->
<gear x="-2.79" y="-1.81" z="-2.20" compression="0.8" spring="1.0">
<gear x="-2.79" y="-1.81" z="-2.20" compression="0.8" spring="1.0" damp="3">
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
<control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>