Fulqrum Publishing Home   |   Register   |   Today Posts   |   Members   |   UserCP   |   Calendar   |   Search   |   FAQ

Go Back   Official Fulqrum Publishing forum > Fulqrum Publishing > IL-2 Sturmovik: Cliffs of Dover

IL-2 Sturmovik: Cliffs of Dover Latest instalment in the acclaimed IL-2 Sturmovik series from award-winning developer Maddox Games.

 
 
Thread Tools Display Modes
Prev Previous Post   Next Post Next
  #25  
Old 05-31-2011, 01:14 PM
ARM505 ARM505 is offline
Approved Member
 
Join Date: Apr 2010
Posts: 41
Default

I'll ask my question another way.

I'm comparing two different models (FSX vs CLOD), both of a Spit MkII with a constant speed propeller:

1) The A2A simulations Spit Mk II running in FSX. In this model, whilst flying at a constant altitude, constant airspeed, constant throttle setting, the indicated boost will DECREASE when you move the prop control lever to DECREASE RPM - the A2A docs mention that since the supercharger is now being driven at a lower RPM, the indicated boost will decrease. The decrease is however very slight.

http://shockwaveproductions.com/

2) The CLOD model, which (under the same conditions), will show an INCREASE in indicated boost when the RPM is commanded to a lower value via the propeller control lever, ie the opposite of the A2A model in FSX.

Since they display the opposite behaviour, one is therefore correct, and the other incorrect. My question is thus which is most true to life. The A2A Spit is widely recognised as a very well modelled aircraft in FSX terms. I have in the past accepted it's behaviour (with the exception of the rapid wear issues) as well modelled. I would like to find out if this is true in this respect.
Reply With Quote
 


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off

Forum Jump


All times are GMT. The time now is 09:06 AM.


Powered by vBulletin® Version 3.8.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright © 2007 Fulqrum Publishing. All rights reserved.