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.

Reply
 
Thread Tools Display Modes
  #1  
Old 05-10-2012, 02:03 PM
Widow17 Widow17 is offline
Approved Member
 
Join Date: Mar 2011
Posts: 64
Default

i think spits smallest and fastest turn are at about same speed, 109 samllest turn is at a slower speed than its fastest, thats why spits tend to be called easier as you dont have to watch geometrics as much (know when priority drifts to smaller and slower or faster and wider turn)
Reply With Quote
  #2  
Old 05-10-2012, 03:01 PM
Shadylurker Shadylurker is offline
Approved Member
 
Join Date: Feb 2008
Posts: 17
Default

Dynamic stall

Last edited by KG26_Alpha; 05-10-2012 at 10:27 PM. Reason: Image off topic
Reply With Quote
  #3  
Old 05-10-2012, 06:46 PM
Buchon Buchon is offline
Approved Member
 
Join Date: Apr 2011
Posts: 437
Default

Lolz

A nice video, the reproduction of the vortex produced by the Dynamic Stall

Reply With Quote
  #4  
Old 05-10-2012, 08:48 PM
41Sqn_Stormcrow
Guest
 
Posts: n/a
Default

From seeing the cfm clip: That is for me the definition of stall: the breakdown of flow on top of the wing. I do not know of any other definition of stall.

So can somebody explain to me what's so special about dynamic stall?
Reply With Quote
  #5  
Old 05-10-2012, 08:55 PM
ATAG_Colander ATAG_Colander is offline
Approved Member
 
Join Date: Jan 2012
Posts: 214
Default

From http://en.wikipedia.org/wiki/Stall_%28flight%29

Quote:
Dynamic stall is a non-linear unsteady aerodynamic effect that occurs when airfoils rapidly change the angle of attack. The rapid change can cause a strong vortex to be shed from the leading edge of the aerofoil, and travel backwards above the wing. The vortex, containing high-velocity airflows, briefly increases the lift produced by the wing. As soon as it passes behind the trailing edge, however, the lift reduces dramatically, and the wing is in normal stall
Reply With Quote
  #6  
Old 05-10-2012, 09:30 PM
Kurfürst Kurfürst is offline
Approved Member
 
Join Date: Oct 2007
Posts: 705
Default

There she blows!
__________________
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

Last edited by KG26_Alpha; 05-10-2012 at 10:28 PM. Reason: Image off topic
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 07:21 PM.


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