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
  #11  
Old 06-23-2012, 01:36 PM
bongodriver's Avatar
bongodriver bongodriver is offline
Approved Member
 
Join Date: Mar 2011
Location: United Kingdom
Posts: 2,546
Default

.....I dunno, just wanted to get on the winking bandwaggon.
__________________


Intel Q9550 @3.3ghz(OC), Asus rampage extreme MOBO, Nvidia GTX470 1.2Gb Vram, 8Gb DDR3 Ram, Win 7 64bit ultimate edition
Reply With Quote
  #12  
Old 06-23-2012, 03:18 PM
Osprey's Avatar
Osprey Osprey is offline
Approved Member
 
Join Date: Jan 2010
Location: Gloucestershire, England
Posts: 1,264
Default

Quote:
Originally Posted by Kurfürst View Post
Well TsaGi actually measured their Bf 109G-2 a bit faster than the German 'official' specs...
And it's that which you decided to publish as actuals on your website.......
Reply With Quote
  #13  
Old 06-23-2012, 04:08 PM
Plt Off JRB Meaker's Avatar
Plt Off JRB Meaker Plt Off JRB Meaker is offline
Approved Member
 
Join Date: Mar 2011
Location: Windsor,UK
Posts: 864
Default

Quote:
Originally Posted by bongodriver View Post
.....I dunno, just wanted to get on the winking bandwaggon.
Yeah.....there's plenty of winkers on here
__________________
http://i1098.photobucket.com/albums/g374/fastted/82%20Squadron%20Banner.jpg

Alienware Aurora|Win 7 64-bit Home Premium|IC i7-920 Processor (Quad-Core)|14GB DDR3 RAM|1 TB SATA 7200rpm Hard Drive|GIGABYTE GeForce GTX 770 2GB WINDFORCE 3 X fan|Thrustmaster Warthog|Saitek Pro Combat rudder pedals,throttle quadrant and Cessna trim wheel|TrackIR4|Sense of humour,I find it comes in handy!
Reply With Quote
  #14  
Old 06-23-2012, 05:21 PM
Kurfürst Kurfürst is offline
Approved Member
 
Join Date: Oct 2007
Posts: 705
Default

Quote:
Originally Posted by Osprey View Post
And it's that which you decided to publish as actuals on your website.......
Problem? The first test published on the 109G the website were actually the worst ones (WNr. 14 026). You have there the worst and best tests, and everything between them.
__________________
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
  #15  
Old 06-23-2012, 06:38 PM
Osprey's Avatar
Osprey Osprey is offline
Approved Member
 
Join Date: Jan 2010
Location: Gloucestershire, England
Posts: 1,264
Default

Which ones do you believe?
Reply With Quote
  #16  
Old 06-23-2012, 06:51 PM
Kurfürst Kurfürst is offline
Approved Member
 
Join Date: Oct 2007
Posts: 705
Default

Quote:
Originally Posted by Osprey View Post
Which ones do you believe?
Well, personally I believe the official specs (given with +/- 3% tolerance) are in good agreement with most tests, see Erla trials of 13 serial production airframes in avarage almost exactly macth the official figures; this is also true for the Soviet trials.

The rest are also well within this +/- 3% production tolerance, given variations in equipment etc.
__________________
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
  #17  
Old 06-23-2012, 10:53 PM
Crumpp's Avatar
Crumpp Crumpp is offline
Approved Member
 
Join Date: Feb 2008
Posts: 1,552
Default

Quote:
A. S. Nikolay Gerasimovich, sometime relatively long ago I was speaking with a pilot—a frontline veteran. Right after the war they flew in captured aircraft. And no matter how hard they tried, they were unable to attain the speeds the Germans had written in their specifications. The shortfall in speed was significant. In the end, they prevailed upon a German, a high-level specialist, and asked him, “Why this shortfall in speed? Are we using the engine’s capability incorrectly?” His response was that they would never achieve the target speed, because the German specifications showed the theoretical speed, and they were attempting to attain that speed on their instruments.

Nikolay Gerasimovich, in your view, is this possible?

N. G. Of course. We had a group of specialists with us from NII VVS. They were examining specifications and were looking at speed. “What speed is indicated at 7,000 meters? 780? Take away 100. And what about 3,000 meters? 700? Reduce it 70 km.” This is how they calculated the instrumented speed and, characteristically, almost always hit their target. Perhaps they knew something about our focus on speed.
zipper hit the nail on the head.

Yes, they are talking about the difference between indicated airspeed and true airspeed.

Here the Germans relate they will not see the performance on the Kennblatt curves (Vwck or TAS) on the airplanes airspeed indicator (Va or IAS).

Quote:
His response was that they would never achieve the target speed, because the German specifications showed the theoretical speed, and they were attempting to attain that speed on their instruments.
Here TASGI or the manufacturer is attaining the airspeed calibration curves for instrument error.

Quote:
We had a group of specialists with us from NII VVS. They were examining specifications and were looking at speed. “What speed is indicated at 7,000 meters? 780? Take away 100. And what about 3,000 meters? 700? Reduce it 70 km.” This is how they calculated the instrumented speed and, characteristically, almost always hit their target. Perhaps they knew something about our focus on speed.
No conspiracty theory required!!!

As for the state of German aerodynamics, I posted the following articles from the American Institute of Aeronautics and Astronautics library for you guys to enjoy!
Attached Files
File Type: zip german Aerodynamic technology.zip (5.08 MB, 9 views)
File Type: zip German Swept Wing Research1.zip (4.07 MB, 5 views)
Reply With Quote
  #18  
Old 06-24-2012, 02:12 AM
Crumpp's Avatar
Crumpp Crumpp is offline
Approved Member
 
Join Date: Feb 2008
Posts: 1,552
Default

http://www.nar-associates.com/techni...ide_screen.pdf
Reply With Quote
  #19  
Old 06-24-2012, 03:01 AM
ATAG_Doc ATAG_Doc is offline
Approved Member
 
Join Date: May 2010
Location: A brothel in the Mekong Delta
Posts: 1,546
Default

I read inferiority complex.
Reply With Quote
  #20  
Old 06-24-2012, 12:43 PM
5./JG27.Farber 5./JG27.Farber is offline
Approved Member
 
Join Date: Aug 2011
Posts: 1,958
Default

Quote:
Originally Posted by Osprey View Post
I think you need to prove that.
I think YOU need to prove it.



The TAS or IAS makes good sense to me.

Last edited by 5./JG27.Farber; 06-24-2012 at 03:01 PM.
Reply With Quote
Reply

Thread Tools
Display Modes

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 01:21 AM.


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