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Updated FDM, renamed as well for the  66. Changes reflected in the set file

r66-yasim.xml

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