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 > Technical threads > FM/DM threads

FM/DM threads Everything about FM/DM in CoD

Reply
 
Thread Tools Display Modes
  #1  
Old 09-24-2012, 03:19 PM
Crumpp's Avatar
Crumpp Crumpp is offline
Approved Member
 
Join Date: Feb 2008
Posts: 1,552
Default

Quote:
That is obviously wrong
Do the math....
__________________
Reply With Quote
  #2  
Old 09-25-2012, 06:52 AM
JtD JtD is offline
Il-2 enthusiast & Moderator
 
Join Date: Oct 2007
Posts: 903
Default

The 12lb boost calculation done by the RAE is an absolutely reasonable extrapolation.
Reply With Quote
  #3  
Old 09-25-2012, 07:16 AM
Kurfürst Kurfürst is offline
Approved Member
 
Join Date: Oct 2007
Posts: 705
Default

Quote:
Originally Posted by JtD View Post
The 12lb boost calculation done by the RAE is an absolutely reasonable extrapolation.
I have my doubts about it having been made by RAE. It's an obvious farce.
__________________
Il-2Bugtracker: Feature #200: Missing 100 octane subtypes of Bf 109E and Bf 110C http://www.il2bugtracker.com/issues/200
Il-2Bugtracker: Bug #415: Spitfire Mk I, Ia, and Mk II: Stability and Control http://www.il2bugtracker.com/issues/415

Kurfürst - Your resource site on Bf 109 performance! http://kurfurst.org
Reply With Quote
  #4  
Old 09-25-2012, 01:24 PM
Crumpp's Avatar
Crumpp Crumpp is offline
Approved Member
 
Join Date: Feb 2008
Posts: 1,552
Default

Quote:
The 12lb boost calculation done by the RAE is an absolutely reasonable extrapolation.

Well, then walk us through the explaination of how the engine data aligns with the graph. I would love to hear it.

Performance graph showing FTH of 11,000 ft:

http://www.spitfireperformance.com/s...-rae-12lbs.jpg

Engine data with RAM effect at max level speed showing FTH of 8,500 feet:

http://www.spitfireperformance.com/merlin3curve.jpg
__________________
Reply With Quote
  #5  
Old 09-25-2012, 01:59 PM
41Sqn_Banks 41Sqn_Banks is offline
Approved Member
 
Join Date: Oct 2007
Posts: 644
Default

Quote:
Originally Posted by Crumpp View Post
Well, then walk us through the explaination of how the engine data aligns with the graph. I would love to hear it.

Performance graph showing FTH of 11,000 ft:

http://www.spitfireperformance.com/s...-rae-12lbs.jpg

Engine data with RAM effect at max level speed showing FTH of 8,500 feet:

http://www.spitfireperformance.com/merlin3curve.jpg
Let's have a look at +6.25 boost ...

FTH at 17,000 ft (http://www.spitfireperformance.com/merlin3curve.jpg)
Max level speed at 19,000 ft (http://www.spitfireperformance.com/s...-rae-12lbs.jpg)

Looks like max level speed is achieved 2,000 feet above the FTH. Pretty much in line with the difference for +12 boost.

Edit: I want to make clear that this 2,000 ft difference between FTH and max speed must not be present in reality, it's more a systematical difference between the two charts that must be considered when they are compared.

Last edited by 41Sqn_Banks; 09-25-2012 at 02:05 PM.
Reply With Quote
  #6  
Old 09-25-2012, 02:35 PM
Crumpp's Avatar
Crumpp Crumpp is offline
Approved Member
 
Join Date: Feb 2008
Posts: 1,552
Default

That chart was not used because it does not align. The engine chart you linked already includes RAM effect at Vmax.


That means the FTH should match. Not be close or have the same margin of error, but match if that is the correct engine data.

I used the power figures as listed in the flight reports NOT a seperate engine curve that does not match the performance data.
__________________
Reply With Quote
  #7  
Old 09-25-2012, 02:38 PM
Crumpp's Avatar
Crumpp Crumpp is offline
Approved Member
 
Join Date: Feb 2008
Posts: 1,552
Default

__________________
Reply With Quote
  #8  
Old 09-25-2012, 05:06 PM
JtD JtD is offline
Il-2 enthusiast & Moderator
 
Join Date: Oct 2007
Posts: 903
Thumbs down

Quote:
Originally Posted by Crumpp View Post
Engine data with RAM effect at max level speed showing FTH of 8,500 feet:
It's not with ram effect. That's painfully obvious from all the engine and plane data on 6.25lbs around. The power level generated by the engine on this chart has the designation "all out level" and that's all there is to it. Assuming otherwise is like assuming "combat" power is only available when the aircraft is in actual combat.

Last edited by JtD; 09-25-2012 at 05:09 PM.
Reply With Quote
  #9  
Old 09-25-2012, 06:42 PM
41Sqn_Banks 41Sqn_Banks is offline
Approved Member
 
Join Date: Oct 2007
Posts: 644
Default

Quote:
Originally Posted by JtD View Post
It's not with ram effect. That's painfully obvious from all the engine and plane data on 6.25lbs around. The power level generated by the engine on this chart has the designation "all out level" and that's all there is to it. Assuming otherwise is like assuming "combat" power is only available when the aircraft is in actual combat.
You are right, e.g. AP 1590B states 890 bhp at sea level and 1030 bhp at 16,250 ft for +6.25 and 3,000 rpm. The chart is obviously without RAM effect.
Reply With Quote
  #10  
Old 09-25-2012, 05:01 PM
JtD JtD is offline
Il-2 enthusiast & Moderator
 
Join Date: Oct 2007
Posts: 903
Default

Quote:
Originally Posted by Kurfürst View Post
I have my doubts about it having been made by RAE. It's an obvious farce.
I agree it looks simplistic, but technically it is sound and I see no reason it not being an original document. No reason for it being one either, but I will accept it on face value as I see no reason to mistrust Mr.Williams on this issue. If you have more than a gut feeling, I'm willing to re-evaluate my opinion.

Last edited by JtD; 09-25-2012 at 05:07 PM.
Reply With Quote
Reply


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 04:03 PM.


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