Fix from Dave Perry. The wing Z coordinate was inverted in the original
version. This is a low wing aircraft. ;)
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1 changed files with 3 additions and 9 deletions
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@ -28,7 +28,7 @@
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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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<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="6" peak="1.5"/>
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<flap0 start="0.04" end="0.38" lift="1.5" drag="1.2"/>
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@ -44,7 +44,7 @@
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<control-speed control="FLAP0" transition-time="5"/>
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</wing>
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<hstab x="-18.12" y="0.41" z="0.27" length="3.5" effectiveness="2.00"
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<hstab x="-18.12" y="0.41" z="0.27" length="3.5" effectiveness="2.4"
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chord="3" taper=".545" sweep="15">
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<stall aoa="18" width="3" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
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@ -99,13 +99,9 @@
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<control-input axis="/controls/tailwheel-castering" control="CASTERING"/>
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</gear>
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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-input axis="/controls/parking-brake" control="BRAKE"/>
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<control-input axis="/controls/brakes[0]" control="BRAKE"/>
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<!-- <control-input axis="/controls/rudder" control="BRAKE" square="1"
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src0="-1" src1="1" dst0="0.5" dst1="-0.5"/> -->
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<control-input axis="/controls/gear-down" control="EXTEND"/>
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<control-speed control="EXTEND" transition-time="7"/>
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<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
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@ -114,8 +110,6 @@
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<gear x="-6.08" y="-2.52" z="-3.49" compression="1" retract-time="7">
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<control-input axis="/controls/parking-brake" control="BRAKE"/>
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<control-input axis="/controls/brakes[1]" control="BRAKE"/>
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<!-- <control-input axis="/controls/rudder" control="BRAKE" square="1"
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src0="-1" src1="1" dst0="-0.5" dst1="0.5"/> -->
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<control-input axis="/controls/gear-down" control="EXTEND"/>
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<control-speed control="EXTEND" transition-time="7"/>
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<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
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@ -125,6 +119,6 @@
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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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<ballast x="-18.0" y="0.0" z="0.6" mass="-2800"/> <!-- move CG forward -->
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<ballast x="-18.0" y="0.0" z="0.6" mass="-2000"/> <!-- move CG forward -->
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</airplane>
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