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USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby IAHM-COL » Mon Feb 02, 2015 5:07 pm

CONFIRMED AIRCRAFT

The list post here may still develop further. I had been notified of the following "marriages", meaning, that attendees might prepare installing this aircraft in order to prevent yellow gliders :P

Best,
IHCOL



Other Aircrafts modified by The USA Tour Ready Consortium that will be available

  • Panavia Tornado (Recon)
  • Handley Page Victor
Last edited by IAHM-COL on Fri Feb 20, 2015 6:27 pm, edited 11 times in total.
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby onox » Mon Feb 02, 2015 5:45 pm

According to the description, the flightgear-aircraft git repository should not be used. Better link to http://sourceforge.net/p/flightgear/fga ... /Aircraft/ instead.
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby IAHM-COL » Mon Feb 02, 2015 6:01 pm

@ONOX

I don't know who came with such idea, but IMHO is a bad one
Ditching GIT over Subversion!?!

I any case, I dont see "the description" indicating the gitorious should not be used. I succesfully downloaded planes from the gitorious packed individually as log above, but in the SVN you link you either get the whole package or none at all.
It seem a waste of bandwith to get 200+ planes to download a few.

In the meantime I keep linking to the gitorious of individual aircrafts as above, and will look forward to FG admins to straight their path of what is logical when it come to distributing these large databases of planes.

Best,
IHCOL
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby onox » Mon Feb 02, 2015 6:09 pm

See this https://gitorious.org/flightgear-aircraft link. Yes, I know subversion is stupid, but you can checkout specific airplanes with svn, for example:

Code: Select all
svn checkout svn://svn.code.sf.net/p/flightgear/fgaddon/trunk/Aircraft/p51d


Unfortunately svn is now the place where development of the fgdata aircraft happen. Branches and contributions via merge requests have now become impossible. A much better idea would be to keep the aircraft in separate git repositories just like the old and unused flightgear-aircraft repository does it, but apparently the core devs have decided to switch over to svn. But you can always provide resistance by keeping your own planes in git at github or gitorious... which is what I do too.
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby IAHM-COL » Mon Feb 02, 2015 6:15 pm

Thanks for the link to SVN too
SVN!? Not me. Guarantee! GIT is the master, IMHO.

Now the link does point to gitorious, not SVN


DO NOT USE THESE REPOSITORIES. THEY ARE FOR TESTING PURPOSE ONLY
Go to http://gitorious.org/fg/fgdata for the current development repository, including aircraft

ie, the difference is what repository in gitorious is being pointed too. Not a recommendation to go SVN!
Now that is a correction I could make for the links above, but the fg/fgdata one doesnt provide a direct download link to get that single aircraft :? GOOD ONE :D

And again, I say. Whomever is the one for the last choices (ie ffjth or those in the admin realm!) I hope they just make the right choices.
For the purposes of link above, anyone can get the models anyway they feel confortable with, being GIT, SVN, ZIPs etc. :)
Last edited by IAHM-COL on Mon Feb 02, 2015 8:34 pm, edited 3 times in total.
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby IAHM-COL » Mon Feb 02, 2015 6:17 pm

onox wrote in Mon Feb 02, 2015 6:09 pm: Branches and contributions via merge requests have now become impossible.


:?: :?:
We may be in parallel universes! :P
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby onox » Mon Feb 02, 2015 6:19 pm

IAHM-COL wrote in Mon Feb 02, 2015 6:15 pm:Thanks for the link to SVN too
SVN!? Not me. Guarantee! GIT's master.


Good. Can you make sure you also use descriptive commit messages? :wink: Reading messages like "020215-1" makes it hard to follow what is going on.

IAHM-COL wrote in Mon Feb 02, 2015 6:17 pm:
onox wrote in Mon Feb 02, 2015 6:09 pm: Branches and contributions via merge requests have now become impossible.


:?: :?:
We may be in parallel universes! :P


You enjoy branches and merges in svn? :o
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby IAHM-COL » Mon Feb 02, 2015 6:25 pm

onox wrote in Mon Feb 02, 2015 6:19 pm:Good. Can you make sure you also use descriptive commit messages? :wink: Reading messages like "020215-1" makes it hard to follow what is going on.

:P sorry to bother you with the commit messages. If needed, click on the message on github, and you will see a full diff description. Otherwise, my recomm is get a pull :D
The message system I use is asinine, perhaps, just says date an a incremental index. Few exceptions.

onox wrote in Mon Feb 02, 2015 6:19 pm:You enjoy branches and merges in svn? :o

SVN? My favorite piece of ... :mrgreen: distributed revision control system. I guess I misinterpreted you: Now I think we are in same page. Git's easy. SVN is.. <<WHY!? why this?!>>
Last edited by IAHM-COL on Mon Feb 02, 2015 7:37 pm, edited 1 time in total.
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby onox » Mon Feb 02, 2015 6:38 pm

IAHM-COL wrote in Mon Feb 02, 2015 6:25 pm:
onox wrote in Mon Feb 02, 2015 6:19 pm:Good. Can you make sure you also use descriptive commit messages? :wink: Reading messages like "020215-1" makes it hard to follow what is going on.

:P sorry to bother you with the commit messages. If needed, click on the message on github, and you will see a full diff description. Otherwise, my recomm is get a pull :D
The message system I use is asinine, perhaps, just says date an a incremental index. Few exceptions.


It's cumbersome to have to scan the whole commit diff to get an idea what was changed by a commit, so please use better commit messages.

IAHM-COL wrote in Mon Feb 02, 2015 6:25 pm:
onox wrote in Mon Feb 02, 2015 6:19 pm:You enjoy branches and merges in svn? :o

SVN? My favorite piece of ... :mrgreen: distributed revision control system. I guess I misinterpreted you: Now I think we are in same page. Git's easy. SVN is.. <<WHY!? why this?!>>


Uhm... SVN is not distributed, it's centralized. That's why it sucks so much.
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby IAHM-COL » Mon Feb 02, 2015 7:29 pm

onox wrote in Mon Feb 02, 2015 6:38 pm:It's cumbersome to have to scan the whole commit diff to get an idea what was changed by a commit, so please use better commit messages.

OK.
WILCOnsider
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby onox » Mon Feb 02, 2015 8:52 pm

Thanks! :mrgreen:
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby CA1012_Falcon5 » Tue Feb 03, 2015 4:39 am

IAHM-COL wrote in Mon Feb 02, 2015 5:07 pm:CONFIRMED AIRCRAFT

The list post here may still develop further. I had been notified of the following "marriages", meaning, that attendees might prepare installing this aircraft in order to prevent yellow gliders :P

Best,
IHCOL



Other Aircrafts modified by The USA Tour Ready Consortium that will be available

  • Panavia Tornado (Recon)
  • Handley Page Victor


i am not shure on what i am taking just yet COL, so dont jump to conclusions.
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby IAHM-COL » Tue Feb 03, 2015 4:48 am

Roger. You had been move to undecided aircraft. I thought we spoke about the Nene on Mumble... or so I recall... but that's fine ;)
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby LesterBoffo » Tue Feb 03, 2015 5:58 pm

Image

I'm still thinking I'll fly the SeaHawk 2T.
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Re: USA TOUR Event | SAT FEB 21ST 17:00 - 24:00 UTC

Postby LesterBoffo » Tue Feb 03, 2015 9:03 pm

I've done some work on the DH-106 Comet, that was having AP pitch issues with low fuel levels. It's too pretty to not include in this flight. The AP is tamed, and I've added 4800 pounds of additional fuel in two extra tanks.

since all the work is done in the YAsim FDM and the Base .xml I'll post these here to copy.

dh106yasim..
Code: Select all
<?xml version="1.0" encoding="UTF-8"?>

<!-- de Havilland DH 106 Comet 4 : 2011 BARANGER Emmanuel


     Source       : http://en.wikipedia.org/wiki/De_Havilland_Comet

     wingspan     :  35.00 m     ( 114 ft 10 in )
     length       :  33.99 m     ( 111 ft 6 in  )
     height       :   8.99 m     (  29 ft 6 in  )
     Moteurs      : 4 Rolls-Royce Spey turbofans ( 12160 lbf each )
     Empty weight : 75400 lb     ( 34200 kg )
     Cruise speed :    846 km/h  (   457 kt     )
-->

<airplane mass="75400">

  <!-- Approach configuration -->
  <approach speed="120" aoa="5" fuel="0.37">
    <control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
    <control-setting axis="/controls/engines/engine[1]/throttle" value="0.2"/>
    <control-setting axis="/controls/engines/engine[2]/throttle" value="0.2"/>
    <control-setting axis="/controls/engines/engine[3]/throttle" value="0.2"/>
    <control-setting axis="/controls/engines/engine[0]/reheat" value="0"/>
    <control-setting axis="/controls/engines/engine[1]/reheat" value="0"/>
    <control-setting axis="/controls/engines/engine[2]/reheat" value="0"/>
    <control-setting axis="/controls/engines/engine[3]/reheat" value="0"/>
    <control-setting axis="/controls/flight/flaps" value="0.5"/>
    <control-setting axis="/surface-positions/flap-pos-norm" value="0.5"/>
    <control-setting axis="/controls/gear/gear-down" value="1"/>
  </approach>

  <!-- Cruise configuration -->
  <cruise speed="429" alt="44000" fuel="0.7">
    <control-setting axis="/controls/engines/engine[0]/throttle" value="0.75"/>
    <control-setting axis="/controls/engines/engine[1]/throttle" value="0.75"/>
    <control-setting axis="/controls/engines/engine[2]/throttle" value="0.75"/>
    <control-setting axis="/controls/engines/engine[3]/throttle" value="0.75"/>
    <control-setting axis="/controls/engines/engine[0]/reheat" value="0"/>
    <control-setting axis="/controls/engines/engine[1]/reheat" value="0"/>
    <control-setting axis="/controls/engines/engine[2]/reheat" value="0"/>
    <control-setting axis="/controls/engines/engine[3]/reheat" value="0"/>
    <control-setting axis="/controls/flight/flaps" value="0"/>
    <control-setting axis="/controls/gear/gear-down" value="0"/>
  </cruise>

  <cockpit x="16.600" y="0.438" z="-0.710"/>

  <!-- fuselage -->
  <fuselage ax="18.169" ay=" 0.000" az="-1.521" bx=" 12.463" by=" 0.000" bz="-1.1375" width="3.336" taper="0.22" midpoint="1"/>
  <fuselage ax="12.463" ay=" 0.000" az="-1.1375" bx="-4.831" by="0.000" bz="-1.1146" width="3.348" taper="1.0" midpoint="0.5" cy="47.0" cz="47.0"/>
  <fuselage ax="-4.831" ay=" 0.000" az="-1.1146" bx="-15.6745" by=" 0.000" bz="0.5606" width="3.348" taper="0.21" midpoint="0" cy="34.4" cz="34.4"/>

  <!-- Engines left -->
  <fuselage ax=" 4.824" ay=" 3.673" az="-2.372" bx=" -4.497" by="2.875"  bz="-2.388" width="1.1900" taper="0.9" midpoint="0" cy="2.4" cz="6"/>
  <fuselage ax=" 5.467" ay=" 2.158" az="-2.38" bx=" -4.74" by=" 2.885" bz="-2.388" width="1.1900" taper="0.9" midpoint="0" cy="2.4" cz="6"/>

  <!-- Engines right -->
  <fuselage ax=" 5.467" ay="-2.158" az="-2.38" bx=" -4.74" by="-2.885" bz="-2.388" width="1.1900" taper="0.9" midpoint="0" cy="2.4" cz="6"/>
  <fuselage ax=" 4.824" ay="-3.673" az="-2.372" bx=" -4.497" by="-2.875" bz="-2.388" width="1.1900" taper="0.9" midpoint="0" cy="2.4" cz="6"/>

  <!-- Wing tanks -->
<!-- Left tank -->
<fuselage ax="-3.5233" ay="12.4301" az="-2.095" bx="-0.0297" by="12.4301" bz="-0.0949"
          width="1.185" taper="0.3" midpoint="0.53" />
<!-- Right tank -->
<fuselage ax="-3.5233" ay="-12.4301" az="-2.095" bx="-0.0297" by="-12.4301" bz="-0.0949"
          width="1.185" taper="0.3" midpoint="0.53" />

  <wing x="1.512" y="1.67" z="-2.494"
        chord="8.805"
        length="17"
        taper="0.30"
        incidence="1.2"
        twist="-0.9"
        sweep="15"
        dihedral="3"
        camber="0.04">
        <stall aoa="18" width="6" peak="3"/>
        <flap0 start="0.05" end="0.64" lift="1.6" drag="1.8"/>
        <flap1 start="0.64" end="1" lift="1.3" drag="1.1"/>
        <slat start="0" end="1" aoa="5" drag="1.2"/>
        <spoiler start="0.35" end="0.50" lift="0.3" drag="3.0"/>

        <control-input axis="/controls/flight/spoilers" control="SPOILER"/>
        <control-input axis="/controls/flight/flaps" control="FLAP0"/>
        <control-input axis="/surface-positions/flap-pos-norm" control="SLAT"/>
        <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
        <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>

        <control-output control="SPOILER" prop="/surface-positions/speedbrake-pos-norm"/> 
        <control-output control="FLAP0" prop="/surface-positions/flaps-pos-norm"/>
        <control-output control="FLAP0" prop="/surface-positions/slats"/>
        <control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-pos-norm"/>
        <control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-pos-norm"/>

        <control-speed control="FLAP0" transition-time="10"/>
        <control-speed control="SPOILER" transition-time="5"/>
  </wing>

  <hstab x="-13.584" y="0" z="-0.481"
         chord="3.749"
         length="7.235"
         taper="0.46"
         effectiveness="1.48"
         camber="0.01"
         sweep="5"
         dihedral="10">
         <stall aoa="20" width="5" peak="2.5"/>
         <flap0 start="0" end="1" lift="1.35" drag="1.1"/>

         <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"/>
  </hstab>

  <vstab x="-13.900" y="0.00" z="-0.669"
         chord="3.752"
         length="5.230"
         taper="0.30"
         sweep="0">
         <stall aoa="22" width="7" peak="3.5"/>
         <flap0 start="0" end="1" lift="1.3" drag="1.1"/>

         <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
         <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>

         <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm" min="1" max="-1"/>
  </vstab>

  <!-- Engines   source            : http://en.wikipedia.org/wiki/Rolls-Royce_Avon

                 name              : Rolls-Royce Avon
                 type              : Turbojet
                 power cruise      : 12690 lbf dry/16360 lbf with reheat
                 weight            : 2890 lb (1310 kg)
  -->
  <!-- Exterior left -->
  <jet x="2.699" y="3.517"  z="-2.364"
       mass="2890"
       thrust="12690"
       afterburner="16360"
       tsfc="0.805"
       epr="5.66">
       <actionpt x="-4.497" y="3.875"  z="-2.388"/>
       <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
       <control-input axis="/controls/engines/engine[0]/reheat" control="REHEAT"/>
  </jet>

  <!-- Interior left -->
  <jet x="2.699" y="2.082"  z="-2.364"
       mass="2890"
       thrust="12690"
       afterburner="16360"
       tsfc="0.805"
       epr="5.66">
       <actionpt x="-3.818" y="2.880"  z="-2.388"/>
       <control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
       <control-input axis="/controls/engines/engine[1]/reheat" control="REHEAT"/>
  </jet>

  <!-- Interior right -->
  <jet x="2.699" y="-2.082"  z="-2.364"
       mass="2890"
       thrust="12690"
       afterburner="16360"
       tsfc="0.805"
       epr="5.66">
       <actionpt x="-4.652" y="-2.880"  z="-2.388"/>
       <control-input axis="/controls/engines/engine[2]/throttle" control="THROTTLE"/>
       <control-input axis="/controls/engines/engine[2]/reheat" control="REHEAT"/>
  </jet>

  <!-- Exterior right -->
  <jet x="2.699" y="-3.517"  z="-2.364"
       mass="2890"
       thrust="12690"
       afterburner="16360"
       tsfc="0.805"
       epr="5.66">
       <actionpt x="-4.497" y="-3.875"  z="-2.388"/>
       <control-input axis="/controls/engines/engine[3]/throttle" control="THROTTLE"/>
       <control-input axis="/controls/engines/engine[3]/reheat" control="REHEAT"/>
  </jet>

  <!-- nose -->
  <gear x="15.733"  y="0.00" z="-4.437"
        compression="0.75"
        spring="0.7"
        damp="4">
        <control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
        <control-input axis="/controls/gear/gear-down" control="EXTEND"/>

        <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>

        <control-speed control="EXTEND" transition-time="7"/>
  </gear>

  <gear x="0.346" y="4.120" z="-4.517"
        compression="1.1"
        spring="1.8">
        <control-input axis="/controls/gear/brake-left" control="BRAKE"/>
        <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
        <control-input axis="/controls/gear/gear-down" control="EXTEND"/>

        <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>

        <control-speed control="EXTEND" transition-time="7"/>
  </gear>

  <gear x="0.346" y="-4.120" z="-4.517"
        compression="1.1"
        spring="1.8">
        <control-input axis="/controls/gear/brake-right" control="BRAKE"/>
        <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
        <control-input axis="/controls/gear/gear-down" control="EXTEND"/>

        <control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>

        <control-speed control="EXTEND" transition-time="7"/>
  </gear>

               <!-- landing gear aero drag right -->
   <vstab x="15.733"  y="0.00" z="-2.837"
             taper="1"
             incidence="0"
             twist="0"
             chord="0.274"
             sweep="0"
             camber="0.0"
             dihedral="0"
             length="1.3">
                   <stall aoa="30"
             width="18"
             peak="5.5"/>
      <flap0 start="0.00"
                end="1"
                lift="-0.19"
                drag="3.06"/>
      <control-input axis="/controls/gear/gear-down"
                            control="FLAP0"/>
      <control-output control="FLAP0"     
                                                 prop="/gear/gear[2]/position-norm"/>
   <control-speed control="FLAP0"
                            transition-time="7" />
                              
   </vstab>

     <!-- landing gear aero drag left -->

   <vstab x="0.346" y="4.120" z="-2.817"
             taper="1"
             incidence="0"
             twist="0"
             chord="0.274"
             sweep="0"
             camber="0.0"
             dihedral="0"
             length="1.3">
                   <stall aoa="30"
             width="18"
             peak="5.5"/>
      <flap0 start="0.00"
                end="1"
                lift="-0.19"
                drag="3.06"/>
      <control-input axis="/controls/gear/gear-down"
                            control="FLAP0"/>
      <control-output control="FLAP0"     
                                                 prop="/gear/gear[1]/position-norm"/>
   <control-speed control="FLAP0"
                            transition-time="7" />
   </vstab>

 <!-- Nose gear aero drag -->

   <vstab  x="0.346" y="-4.120" z="-2.817"
             taper="1"
             incidence="0"
             twist="0"
             chord="0.184"
             sweep="0"
             camber="0.0"
             dihedral="0"
             length="1.093">
                   <stall aoa="30"
             width="18"
             peak="5.5"/>
      <flap0 start="0.00"
                end="1"
                lift="0.10"
                drag="2.86"/>
      <control-input axis="/controls/gear/gear-down"
                            control="FLAP0"/>
      <control-output control="FLAP0"     
                                                 prop="/gear/gear[0]/position-norm"/>
   <control-speed control="FLAP0"
                            transition-time="7" />
   </vstab>

  <tank x="1.86" y=" 0" z="-2.7" jet="true" capacity="17900"/>
  <tank x="1.26" y=" 5.90" z="-2.32" jet="true" capacity="17900"/>
  <tank x="1.26" y="-5.90" z="-2.32" jet="true" capacity="17900"/>
  <tank x="1.665" y=" 12.4301" z="-0.0949" jet="true" capacity="2500"/>
  <tank x="1.665" y="-12.4301" z="-0.0949" jet="true" capacity="2500"/>

  <ballast x="10" y="0" z="-2" mass="8000"/>

</airplane>


dh106 base...
Code: Select all
<?xml version="1.0" encoding="UTF-8"?>

<PropertyList>

  <sim include="Nasal/views.xml">

    <aircraft-version>0.1</aircraft-version>
    <status>Alpha</status>

    <fuel-fraction>1.0</fuel-fraction>

    <startup>
      <splash-texture>Aircraft/DH-106/dh106-splash.png</splash-texture>
    </startup>

    <sound>
      <path archive="y">Aircraft/DH-106/Sounds/dh106-sound.xml</path>
    </sound>

    <model>
      <path archive="y">Aircraft/DH-106/Models/dh106.xml</path>
      <livery>
        <file type="string">default</file>
      </livery>
    </model>

    <multiplay>
      <chat_display>1</chat_display>
      <generic>
        <int type="int" n="0">0</int>
        <int type="int" n="1">0</int>
        <int type="int" n="2">0</int>
        <int type="int" n="3">0</int>
        <int type="int" n="4">0</int>
        <int type="int" n="5">0</int>
        <float n="0" alias="/instrumentation/doors/crew/position-norm"/>
        <float n="1" alias="/instrumentation/doors/passenger/position-norm"/>
      </generic>
    </multiplay>

    <help>
      <title>dh106</title>
      <key>
        <name>d</name>
        <desc>Open/Close door</desc>
      </key>
    </help>

      <!-- Flap detents -->
  <flaps>
    <setting>0.00</setting>
    <setting>0.125</setting> <!-- 5 deg -->
    <setting>0.275</setting> <!-- 11 deg (standard takeoff) -->
    <setting>0.375</setting> <!-- 15 deg (standard takeoff)-->
    <setting>0.5</setting>   <!-- 20 deg -->
    <setting>0.7</setting>   <!-- 28 deg (standard landing) -->
    <setting>1.00</setting>  <!-- 40 deg (standard landing) -->
  </flaps>

    <menubar include="Dialogs/dh106-menu.xml"/>

  </sim>
 
  <input>
    <keyboard include="Nasal/dh106-keyboard.xml"/>
  </input>
 
  <nasal>
    <doors>
      <file>Aircraft/DH-106/Nasal/doors.nas</file>
    </doors>
    <dh106>
      <file>Aircraft/DH-106/Nasal/light.nas</file>
      <file>Aircraft/DH-106/Nasal/liveries.nas</file>
<!--  <file>Aircraft/DH-106/Nasal/immat.nas</file> -->
    </dh106>
  </nasal>
   
</PropertyList>


give it a try and report back I'm not certain about the RR Spey engines on the DH Comet having afterburners, but you can always fly it without the reheat. It's plenty overpowered as it is..
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LesterBoffo
 
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Joined: Sun Oct 02, 2011 4:02 pm
Location: Western USA
Callsign: LesBof
Version: 2016.1
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