CVS: data/Aircraft/DH-88 dh88-yasim.xml, 1.4, 1.5

Update of /var/cvs/FlightGear-0.9/data/Aircraft/DH-88
In directory baron.flightgear.org:/tmp/cvs-serv25653

Modified Files:
	dh88-yasim.xml 
Log Message:
- little update on FDM (thanks to Melchior for the YASim_import script)

Index: dh88-yasim.xml
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/DH-88/dh88-yasim.xml,v
retrieving revision 1.4
retrieving revision 1.5
diff -u -r1.4 -r1.5
--- dh88-yasim.xml	2 Mar 2009 16:46:13 -0000	1.4
+++ dh88-yasim.xml	9 Apr 2010 23:05:54 -0000	1.5
@@ -6,7 +6,7 @@
    Longueur     :  8.8 m        ( 29'0 ft)
    Hauteur      :  3.1 m        ( 10'0 ft)
    Moteurs      : 2 x Gypsy Six (230 cv) 
-   Poids à vide : 1330 kg       ( 2930 lb)
+   Poids a vide : 1330 kg       ( 2930 lb)
    Vitesse max  : 381 km/h      ( 237 mph)
    Alttitude    : 5790 m        ( 19000 ft)
 -->
@@ -41,10 +41,10 @@
 
   <wing x="1.312" y="0.293" z="-0.219" 
         chord="2.343" 
-        taper=".20" 
         length="6.319" 
+        taper=".20" 
         camber="0.1"
-        sweep="2" 
+        sweep="1.5" 
         dihedral="1.5">
         <stall aoa="14" width="6" peak="1.5"/>
         <flap1 start="0.550" end="0.945" lift="1.2" drag="1.2"/>
@@ -58,10 +58,9 @@
 
   <hstab x="-3.504" y="0.0" z="0.391" 
          chord="1.320" 
-         taper="0.22" 
          length="1.851" 
-         sweep="10" 
-         incidence="0">
+         taper="0.22" 
+         sweep="12">
          <stall aoa="18" width="3" peak="1.5"/>
          <flap0 start="0" end="1" lift="1.5" drag="1.2"/>
 
@@ -73,9 +72,9 @@
 
   <vstab x="-3.320" y="0" z="0.248" 
          chord="1.989" 
+         length="1.48"
          taper="0.24" 
-         length="1.262"
-         sweep="35">
+         sweep="30">
          <stall aoa="14" width="3" peak="1.5"/>
          <flap0 start="0" end="1" lift="1.5" drag="1.2"/>
 
@@ -88,8 +87,8 @@
   <!-- Moteur gauche -->
   <propeller x="2.500" y="1.469" z="-0.519"
              mass="600" 
-             moment="35" 
-             radius="1.8"
+             moment="3.5" 
+             radius="0.918"
              cruise-power="200" 
              cruise-speed="195"
              cruise-rpm="2300" 
@@ -109,8 +108,8 @@
   <!-- Moteur droit -->
   <propeller x="2.500" y="-1.469" z="-0.519"
              mass="600" 
-             moment="35" 
-             radius="1.8"
+             moment="3.5" 
+             radius="0.918"
              cruise-power="200" 
              cruise-speed="195"
              cruise-rpm="2300" 
@@ -164,7 +163,7 @@
 
   <tank x="0" y="0.0" z="0.0" capacity="1000"/>
 
-  <!-- CH théorique x=1.312 y=0 z=-0.219 --> 
+  <!-- CH theorique x=1.312 y=0 z=-0.219 --> 
   <ballast x="0.77" y="0.0" z="-0.065" mass="500"/>
 
 </airplane>

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