CVS: data/Aircraft/F-106-dart f106-splash.png, 1.1, 1.2 f106-yasim.xml, 1.1, 1.2 thumbnail.jpg, 1.1, 1.2
Emmanuel Baranger <[email protected]> Sat, 10 Apr 2010 18:02:27 -0500
| Newsgroups | gmane.games.flightgear.cvc |
|---|---|
| Message-ID | <[email protected]> |
Update of /var/cvs/FlightGear-0.9/data/Aircraft/F-106-dart
In directory baron.flightgear.org:/tmp/cvs-serv29804
Modified Files:
f106-splash.png f106-yasim.xml thumbnail.jpg
Log Message:
- update FDM (thanks to Melchior for the YASim_import script)
Index: f106-splash.png
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/F-106-dart/f106-splash.png,v
retrieving revision 1.1
retrieving revision 1.2
diff -u -r1.1 -r1.2
Binary files /tmp/cvsfKHUi3 and /tmp/cvsheCAJo differ
Index: f106-yasim.xml
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/F-106-dart/f106-yasim.xml,v
retrieving revision 1.1
retrieving revision 1.2
diff -u -r1.1 -r1.2
--- f106-yasim.xml 10 Jan 2009 17:01:54 -0000 1.1
+++ f106-yasim.xml 10 Apr 2010 23:02:25 -0000 1.2
@@ -1,23 +1,26 @@
<?xml version="1.0" encoding="UTF-8"?>
-<!--
- Convair F 106 Delta Dart : 2009 BARANGER Emmanuel
+
+<!-- Convair F 106 Delta Dart : 2009 BARANGER Emmanuel
+
+ Source : http://en.wikipedia.org/wiki/F-106_Delta_Dart
- Envergure :
- Longueur :
- Hauteur :
- Masse à vide : 10955 kg (24151 lb)
- Moteur :
- Réservoirs
- Internes : 2 x 2325.5 lb
- Externes : 2 x 4921.5 lb
+ Wingspan : 11.67 m ( 38.25 ft )
+ Length : 21.55 m ( 70.70 ft )
+ Height : 6.18 m ( 20.28 ft )
+ Empty weight : 11077 kg ( 24420 lb )
+ Moteur : Pratt & Whitney J75-17 afterburning turbojet, 24500 lbf.
+ Speed max : Mach 2.3 ( 2455 km/h / 1325.59 kts )
+ Reservoirs
+ Internes : 2 x 4921.5 lb
+ Externes : 2 x 2325.5 lb
-->
-<airplane mass="24151">
+<airplane mass="24420">
<!-- Approach configuration -->
- <approach speed="150" aoa="7">
+ <approach speed="145" aoa="8" fuel="1">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.4"/>
- <control-setting axis="/controls/engines/engine[0]/afterburner" value="0.0"/>
+ <control-setting axis="/controls/engines/engine[0]/afterburner" value="0"/>
<control-setting axis="/controls/flight/flaps" value="0.4"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<control-setting axis="/controls/flight/speedbrake" value="0"/>
@@ -25,70 +28,76 @@
</approach>
<!-- Cruise configuration. -->
- <cruise speed="565" alt="45000">
+ <cruise speed="1200" alt="45000" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.7"/>
- <control-setting axis="/controls/engines/engine[0]/afterburner" value="0.0"/>
- <control-setting axis="/controls/flight/flaps" value="0.0"/>
+ <control-setting axis="/controls/engines/engine[0]/afterburner" value="0"/>
+ <control-setting axis="/controls/flight/flaps" value="0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<control-setting axis="/controls/flight/speedbrake" value="0"/>
<control-setting axis="/controls/flight/slats" value="0"/>
</cruise>
<!-- pilot eyepoint -->
- <cockpit x="4.197" y="0.0" z="-0.150"/>
+ <cockpit x="4.197" y="0" z="-0.150"/>
+
+ <fuselage ax="9.282" ay="0" az="-1.474" bx="-10.213" by="0" bz="-0.429" width="1.8" midpoint= "0.3" taper="0.5" />
- <fuselage ax="10.728" ay="0" az="-0.795" bx="-11.296" by="0" bz="-0.795" width="2.263" midpoint= "0.7" />
+ <!-- Left reservoir -->
+ <fuselage ax="-0.265" ay="2.662" az="-1.981" bx="-7.106" by="2.662" bz="-1.648" width="0.6" midpoint= "0.5" taper="0.5" />
+
+ <!-- Right reservoir -->
+ <fuselage ax="-0.265" ay="-2.662" az="-1.981" bx="-7.106" by="-2.662" bz="-1.648" width="0.5" midpoint= "0.5" taper="0.5" />
<wing x="-3.399" y="0.907" z="-1.129"
chord="9.489"
- length="4.939"
+ length="6.35"
taper="0.035"
- sweep="20"
+ sweep="39.5"
dihedral="-3"
- camber="0.126">
- <stall aoa="21" width="8" peak="1.3"/>
- <flap0 start="0.0" end="0.5" lift="1.2" drag="1.1"/>
- <slat aoa="6" start="0.0" end="0.813" lift="1.8" drag="1.7"/>
- <spoiler start="0.34" end="0.44" lift="-2" drag="15.5"/>
-
- <control-input axis="/controls/flight/aileron" control="FLAP0" split="true"/>
- <control-input axis="/controls/flight/aileron-trim" control="FLAP0" split="true"/>
- <control-input axis="/controls/flight/flaps" control="SLAT"/>
+ camber="0.001">
+ <stall aoa="22" width="1" peak="1.2"/>
+ <flap0 start="0" end="0.813" lift="1.2" drag="1.3"/>
+ <flap1 start="0" end="0.39" lift="1.8" drag="1.7"/>
+ <spoiler start="0.39" end="0.80" lift="1.3" drag="1.3"/>
+
+ <control-input axis="/controls/flight/flaps" control="FLAP0"/>
+ <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
+ <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/spoilers" control="SPOILER"/>
- <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
- <control-output control="SLAT" prop="/surface-positions/slat-pos-norm"/>
+ <control-output control="FLAP0" prop="/surface-positions/slat-pos-norm"/>
+ <control-output control="FLAP1" prop="/surface-positions/flap-pos-norm"/>
<control-output control="SPOILER" prop="/surface-positions/speedbrake-pos-norm"/>
- <control-speed control="SLAT" transition-time="1.1"/>
- <control-speed control="FLAP0" transition-time="1"/>
+ <control-speed control="FLAP0" transition-time="1.1"/>
+ <control-speed control="FLAP1" transition-time="1"/>
<control-speed control="SPOILER" transition-time="1.5"/>
</wing>
- <hstab x="-7.598" y="0.892" z="-1.118"
- chord="1.022"
- length="4.912"
- taper="1"
- dihedral="-3">
- <stall aoa="22" width="13" peak="1.5"/>
- <flap0 start="0" end="1" lift="1.9" drag="1.4"/>
- <flap1 start="0.0" end="0.15" lift="0.0" drag="0.8"/>
+ <hstab x="-3.399" y="0.907" z="-1.129"
+ chord="9.489"
+ length="6.35"
+ taper="0.035"
+ sweep="39.5"
+ dihedral="-3">
+ <stall aoa="22" width="1" peak="1.4"/>
+ <flap0 start="0.0" end="0.40" lift="1.4" drag="1.5"/>
- <control-input axis="/controls/flight/elevator" control="FLAP0"/>
- <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
+ <control-input axis="/controls/flight/elevator" control="FLAP0"/>
+ <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
- <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
+ <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
- <control-speed control="FLAP0" transition-time="4"/>
+ <control-speed control="FLAP0" transition-time="4"/>
</hstab>
<vstab x="-7.486" y="0.0" z="0.141"
chord="4.998"
- length="3.096"
+ length="4.4"
taper="0.28"
- sweep="35">
- <stall aoa="27" width="10" peak="1.5"/>
- <flap0 start="0" end=".8" lift="1.3" drag="1.3"/>
+ sweep="38">
+ <stall aoa="20" width="1" peak="1.2"/>
+ <flap0 start="0.2" end="0.72" lift="1.3" drag="1.4"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
@@ -98,7 +107,15 @@
<control-speed control="FLAP0" transition-time="1"/>
</vstab>
- <!-- Pratt & Whitney J75 axial-flow -->
+ <!-- Pratt & Whitney J75 axial-flow
+
+ Engines source : http://en.wikipedia.org/wiki/Pratt_%26_Whitney_J75
+
+ name : Pratt & Whitney J75-P-17
+ type : Turbojet afterburning thrust
+ thrust : 17200 lb
+ afterburner : 24500 lb
+ -->
<jet x="-3.688" y="0.0" z="-0.749"
mass="4000"
thrust="17200"
@@ -157,20 +174,19 @@
<control-output control="EXTEND" prop="gear/gear[2]/position-norm"/>
</gear>
-
<!-- Internal Tanks weight total : 4465 kg -> 9843 lb -> 2 x 4921.5 -->
- <tank x="-2.5" y="2.3" z="-1.237" jet="true" capacity="4921.5"/>
- <tank x="-2.5" y="-2.3" z="-1.237" jet="true" capacity="4921.5"/>
+ <tank x="-2.4" y="2.3" z="-1.237" jet="true" capacity="4921.5"/>
+ <tank x="-2.4" y="-2.3" z="-1.237" jet="true" capacity="4921.5"/>
<!-- External Tanks weight total : 2110 kg -> 4651 lb -> 2 x 2325.5 -->
- <tank x="-3.727" y="2.658" z="-1.817" jet="true" capacity="2325.5"/>
- <tank x="-3.727" y="-2.658" z="-1.817" jet="true" capacity="2325.5"/>
+ <tank x="-2.727" y="2.658" z="-1.817" jet="true" capacity="2325.5"/>
+ <tank x="-2.727" y="-2.658" z="-1.817" jet="true" capacity="2325.5"/>
<!-- External Tanks empty weight -->
- <weight x="-3.727" y="2.658" z="-1.817" size="0.28" mass-prop="sim/weight[0]/weight-lb"/>
- <weight x="-3.727" y="-2.658" z="-1.817" size="0.28" mass-prop="sim/weight[1]/weight-lb"/>
+ <weight x="-2.727" y="2.658" z="-1.817" size="0.28" mass-prop="sim/weight[0]/weight-lb"/>
+ <weight x="-2.727" y="-2.658" z="-1.817" size="0.28" mass-prop="sim/weight[1]/weight-lb"/>
- <!-- CG Théorique x=-3.399 y=0.0 z=-1.129 -->
- <ballast x="0" y="0" z="0" mass="1000" />
+ <!-- CG Theorique x=-3.399 y=0.0 z=-1.129 -->
+ <ballast x="8.5" y="0" z="-3" mass="2000" />
</airplane>
Index: thumbnail.jpg
===================================================================
RCS file: /var/cvs/FlightGear-0.9/data/Aircraft/F-106-dart/thumbnail.jpg,v
retrieving revision 1.1
retrieving revision 1.2
diff -u -r1.1 -r1.2
Binary files /tmp/cvsRXktH8 and /tmp/cvsP1X6cu differ
------------------------------------------------------------------------------
Download Intel® 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