CVS: data/Aircraft/Skyvan skyvan-splash.png, 1.3, 1.4 skyvan-yasim.xml, 1.2, 1.3

Update of /var/cvs/FlightGear-0.9/data/Aircraft/Skyvan
In directory baron.flightgear.org:/tmp/cvs-serv3355

Modified Files:
	skyvan-splash.png skyvan-yasim.xml 
Log Message:
- new splash screen by Michat. Thanks to him
- update on FDM (thanks to Melchior for the YASim_import script)

Index: skyvan-splash.png
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/Skyvan/skyvan-splash.png,v
retrieving revision 1.3
retrieving revision 1.4
diff -u -r1.3 -r1.4
Binary files /tmp/cvsBlUbKA and /tmp/cvsQGAZSL differ

Index: skyvan-yasim.xml
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/Skyvan/skyvan-yasim.xml,v
retrieving revision 1.2
retrieving revision 1.3
diff -u -r1.2 -r1.3
--- skyvan-yasim.xml	12 Jan 2009 15:37:25 -0000	1.2
+++ skyvan-yasim.xml	31 Mar 2010 17:49:29 -0000	1.3
@@ -1,10 +1,13 @@
 <?xml version="1.0" encoding="UTF-8"?>
+
 <!-- SHORT SC.7 Skyvan : 2008 BARANGER Emmanuel 
 
-     wingspan     : 19.80 m (64 ft 11 in)
-     length       : 12.20 m (40 ft  1 in)
+     sources      : http://en.wikipedia.org/wiki/Short_SC.7_Skyvan
+
+     wingspan     : 19.79 m (64 ft 11 in)
+     length       : 12.21 m (40 ft  1 in)
      height       :  4.60 m (15 ft  1 in)
-     Moteurs      : 2 turboprops Garrett AiResearch TPE-331-201 (715 hp each)
+     Moteurs      : 2 Garrett AiResearch TPE-331-201 Turboprops (715 hp each)
      Empty weight : 3331 kg (7344 lb)
      Cruise speed : 315 km/h (176 kts)
 -->
@@ -33,16 +36,17 @@
 
   <cockpit x="4.452" y="0.584" z="0.192"/>
 
-  <fuselage ax="6.042" ay="0" az="-0.374" bx="-6.050" by="0" bz="-0.374" width="2.369" taper="0.5" midpoint="0.25"/>
+  <fuselage ax="6.053" ay="0" az="-0.944" bx="-5.492" by="0" bz="0.126" width="2.369" taper="0.4" midpoint="0.25"/>
 
   <wing x="1.036" y="1.094" z="0.819" 
         chord="1.837" 
-        length="8.698" 
+        length="8.8" 
         taper="1.0" 
-        camber="0.123">
+        camber="0.124"
+        dihedral="2">
         <stall aoa="16" width="6" peak="1.5"/>
-        <flap0 start="0.019" end="0.620" lift="1.4" drag="1.4"/>
-        <flap1 start="0.620" end="1.000" lift="1.4" drag="1.2"/>
+        <flap0 start="0.019" end="0.650" lift="1.4" drag="1.4"/>
+        <flap1 start="0.650" end="1.000" lift="1.4" drag="1.2"/>
 
         <control-input axis="/controls/flight/flaps" control="FLAP0"/>
         <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
@@ -58,8 +62,7 @@
   <hstab x="-5.411" y="0" z="0.126"
          chord="1.301"
          length="3.000" 
-         taper="1.0"
-         sweep="10">
+         taper="1">
          <stall aoa="14" width="3" peak="1.5"/>
          <flap0 start="0" end="1" lift="1.8" drag="1.9"/>
 
@@ -72,8 +75,7 @@
   <vstab x="-5.387" y="3.018" z="-0.503"
          chord="1.446"
          length="2.855" 
-         taper="1.0"
-         sweep="4">
+         taper="1">
          <stall aoa="12" width="3" peak="1.5"/>
          <flap0 start="0" end="1" lift="1.5" drag="1.5"/>
 
@@ -86,8 +88,7 @@
   <vstab x="-5.387" y="-3.018" z="-0.503"
          chord="1.446"
          length="2.855" 
-         taper="1.0"
-         sweep="4">
+         taper="1">
          <stall aoa="14" width="3" peak="1.5"/>
          <flap0 start="0" end="1" lift="1.5" drag="1.5"/>
 
@@ -97,14 +98,15 @@
          <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
   </vstab>
 
-  <!-- Moteur gauche
-                 
-                                         Rayon * Rayon * Mass(kg)   1.25*1.25 * 487.15
-                 moment d'après la doc : ________________________ = __________________ = 253.72
-                                                     3                      3
+  <!-- Engines   source            : http://en.wikipedia.org/wiki/Garrett_TPE331
+
+                 name              : Garrett AiResearch TPE331
+                 type              : Single-shaft turboprop with integral gearbox
+                 power cruise      : 715 hp
+                 weight            :    336 lb  (153 kg)
   -->
   <propeller x="2.116" y="2.628" z="0.578"
-             mass="1500" 
+             mass="336" 
              moment="253.72" 
              radius="1.25" 
              cruise-speed="176" 
@@ -129,7 +131,7 @@
   </propeller>
 
   <propeller x="2.116" y="-2.628" z="0.578"
-             mass="1500" 
+             mass="336" 
              moment="253.72" 
              radius="1.25" 
              cruise-speed="176" 
@@ -191,7 +193,7 @@
   <tank x="1.03" y="2.5" z="0.57" capacity="1472"/>
   <tank x="1.03" y="-2.5" z="0.57" capacity="1472"/>
 
-  <!-- CG Théorique x=1.036 y=0 z=-1 -->
-  <ballast x="2.0" y="0.0" z="-1.0" mass="1000"/>
+  <!-- CG Theorique x=1.036 y=0 z=-1 -->
+  <ballast x="6" y="0" z="-2" mass="1000"/>
 
 </airplane>

------------------------------------------------------------------------------
Download Intel&#174; Parallel Studio Eval
Try the new software tools for yourself. Speed compiling, find bugs
proactively, and fine-tune applications for parallel performance.
See why Intel Parallel Studio got high marks during beta.
http://p.sf.net/sfu/intel-sw-dev

_______________________________________________
Flightgear-cvslogs mailing list
[email protected]
https://lists.sourceforge.net/lists/listinfo/flightgear-cvslogs