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@@ -24,16 +24,16 @@
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phi0="45"
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maxcollective="13"
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mincollective="0.0"
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- mincyclicele="-17.5"
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- maxcyclicele="17.5"
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+ mincyclicele="-30.5"
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+ maxcyclicele="30.5"
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mincyclicail="-10.5"
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- maxcyclicail="10.7"
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+ maxcyclicail="15.7"
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diameter="10.0584"
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numblades="2"
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weightperblade="40"
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relbladecenter="0.3"
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- dynamic="1"
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- rpm="495"
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+ dynamic="0.8"
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+ rpm="408"
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rellenflaphinge="0.2"
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delta3="0.0"
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delta=".25"
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@@ -45,17 +45,17 @@
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flap0factor="0"
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notorque="0"
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dragfactor="0.30"
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- translift-ve="20"
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- translift-maxfactor="0.3"
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+ translift-ve="5"
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+ translift-maxfactor="0.7"
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ground-effect-constant="0.1"
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- twist="-2"
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- taper="1"
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- chord="0.18288"
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+ twist="-4"
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+ taper="0.95"
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+ chord="0.309"
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number-of-segments="8"
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number-of-parts="8"
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rel-len-where-incidence-is-measured="0.7"
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rel-len-blade-start="0.04"
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- airfoil-lift-coefficient="5.67"
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+ airfoil-lift-coefficient="5.87"
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airfoil-drag-coefficient0="0.01"
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airfoil-drag-coefficient1="0.05"
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incidence-stall-zero-speed="19"
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@@ -107,7 +107,7 @@
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drag-factor-stall="8"
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notorque="0"
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taper="1"
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- chord="0.116"
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+ chord="0.1397"
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number-of-segments="5"
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number-of-parts="4"
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rel-len-blade-start="0.2"
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@@ -121,11 +121,11 @@
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<rotorgear max-power-engine="200"
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max-power-rotor-brake="50"
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- rotorgear-friction="0.5"
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+ rotorgear-friction="0.3"
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engine-prop-factor="0.005"
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engine-accel-limit="3"
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- yasimdragfactor="10"
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- yasimliftfactor="140">
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+ yasimdragfactor="5"
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+ yasimliftfactor="145">
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<control-input axis="/controls/engines/engine[0]/magnetos" control="ROTORGEARENGINEON"/>
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@@ -150,24 +150,26 @@
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chord="0.510"
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length="1.080"
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taper="0.5"
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- sweep="16">
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- <stall aoa="16" width="4" peak="1.5"/>
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+ sweep="16"
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+ incidence="0.5">
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+ <stall aoa="6" width="9" peak="2.3"/>
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</vstab>
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<vstab x="-5.8" y="-0.182" z="0.6"
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chord="0.510"
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length="0.800"
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taper="0.6"
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- dihedral="270"
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- sweep="18">
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- <stall aoa="16" width="4" peak="1.5"/>
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+ dihedral="-90"
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+ sweep="18"
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+ incidence="-0.5">
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+ <stall aoa="6" width="9" peak="2.3"/>
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</vstab>
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<hstab x="-5.8" y="-0.098" z="0.637"
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chord="0.52"
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length="1.15"
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taper="0.5"
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- dihedral="180">
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+ dihedral="0">
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<stall aoa="0" width="0" peak="1.5"/>
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</hstab>
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@@ -239,14 +241,15 @@
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<ballast x="-1" y=" 1.1" z=" 1.1" mass="100"/>
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<ballast x="-1" y="-1.1" z=" 1.1" mass="50"/>
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- <thruster x="0.1" y="0.0" z="1.905" vx="-1" vy="0" vz="1" thrust="850">
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- <control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
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+ <thruster x="0.1" y="0.0" z="1.905" vx="1" vy="0" vz="0" thrust="2000">
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+ <control-input axis="/rotors/main/vibration/longitudinal" src0="-1" src1="1" dst0="-1" dst1="1" control="THROTTLE"/>
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</thruster>
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- <thruster x="0.1" y="0.0" z="1.905" vx="0" vy="1" vz="0" thrust="300">
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- <control-input axis="/sim/model/pushback/target-speed-fps-y" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
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+ <thruster x="0.1" y="0.0" z="1.905" vx="0" vy="1" vz="0" thrust="2000">
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+ <control-input axis="/rotors/main/vibration/lateral" src0="-1" src1="1" dst0="-1" dst1="1" control="THROTTLE"/>
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</thruster>
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+
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</airplane>
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