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FM/DM threads Everything about FM/DM in CoD

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  #1  
Old 12-28-2011, 08:43 PM
5./JG27.Farber 5./JG27.Farber is offline
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Anyway back to this website... (and all the others like it)

I was talking to a Aeronautical engineer over steam (I will let him name himself if he wishes) he basically said something like, "just like any other flight page, this is grains of truth mixed with BS..."

So I guess what we have learned here is that none of the information we ever find will give us definative answears on aircraft performance... These debates of this source said this and that source said that will just continue... Would be nice if we just new the right physics for the game but I suppose it will always be a bit of science and a bit of legend...
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  #2  
Old 12-29-2011, 12:27 AM
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CaptainDoggles CaptainDoggles is offline
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Quote:
Originally Posted by 5./JG27.Farber View Post
Anyway back to this website... (and all the others like it)

I was talking to a Aeronautical engineer over steam (I will let him name himself if he wishes) he basically said something like, "just like any other flight page, this is grains of truth mixed with BS..."
Most flight websites are like this, but there are some good ones out there. You have to be literate in the underlying math and physics to discern between the two, though.

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So I guess what we have learned here is that none of the information we ever find will give us definative answears on aircraft performance... These debates of this source said this and that source said that will just continue... Would be nice if we just new the right physics for the game but I suppose it will always be a bit of science and a bit of legend...
It's always science.

The problem is that aircraft performance is complicated stuff, and this is compounded by the fact that aircraft design was a nascent art at the time. Lessons were still being learned, and they don't necessarily do stuff the same way we do things now.

On top of that, things get lost over the years and much of the available data is incomplete.

Aircraft performance is ideally recorded in conjunction with the atmospheric conditions on the day the test was flown. That data is then converted to standard atmospheric conditions. The data is supposed to represent an idealized aircraft flying in the standard atmosphere, and engineers understand that aircraft performance exists as a range of values within an acceptable tolerance.

Test data can often contradict other test data. Sometimes the reasons for the contradiction can be discovered if there is qualitative data accompanying the test. Often this data does not exist or is insufficient and so the difference cannot be resolved. This is where the "legend' bit comes into play.
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Old 12-29-2011, 01:48 AM
5./JG27.Farber 5./JG27.Farber is offline
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Yes yes. All of these conclusions are what I expected. Gentleman you have been part of an experiment!

You see in the next release we will see FM/DM tweeks... We will see arguments for this and that... Those who back the RAF will be dubbed "fanboise" and those who back the Luftwaffe will be called "Luftwhiners"... So by proposing my information first with a fail we can take a good long hard look at variuos sources and subject them to "our laymen brains" and that of experts - with a pinch of salt and realise we just might be wrong!

Hope this helps avoid any arguments of FM/DM tweeks in the near future!

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Old 12-29-2011, 01:52 AM
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CaptainDoggles CaptainDoggles is offline
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Originally Posted by 5./JG27.Farber View Post
Yes yes. All of these conclusions are what I expected. Gentleman you have been part of an experiment!

You see in the next release we will see FM/DM tweeks... We will see arguments for this and that... Those who back the RAF will be dubbed "fanboise" and those who back the Luftwaffe will be called "Luftwhiners"... So by proposing my information first with a fail we can take a good long hard look at variuos sources and subject them to "our laymen brains" and that of experts - with a pinch of salt and realise we just might be wrong!

Hope this helps avoid any arguments of FM/DM tweeks in the near future!

Good effort, but you're going to be disappointed. Many people have agendas, and the VVS are a particularly polarizing subject.
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Old 12-29-2011, 10:36 AM
Kurfürst Kurfürst is offline
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Rather badly researched and biased article I'd say with a large amount of clear errors, ie. the production number of Bf 109G, no Spitfire Mk V reached 400 mph, and he got it all wrong about the ailerons (109A-E had plain type ailerons, F-K had Frise type ailerons, and all Spits - maybe post-war versions didn't? - had Frise.)

The only really good point is about roll inertia, the 109 indeed seem to have been praised for brisk aileron control (that means, quick response, not neccessarily the same as maximum rate of roll) at low to medium speeds. And of course the 109 benefited from its high-lift devices on the wing in numerous ways, but the main thing about the 109-p51 climb rate difference was obviously that the latter was about a ton heavier.
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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
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Old 12-29-2011, 11:10 AM
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And here's another:
http://www.youtube.com/watch?NR=1&fe...&v=TFl8X4y9-94

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  #7  
Old 12-31-2011, 03:52 AM
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Originally Posted by Kurfürst View Post
Rather badly researched and biased article I'd say with a large amount of clear errors, ie. the production number of Bf 109G, no Spitfire Mk V reached 400 mph, and he got it all wrong about the ailerons (109A-E had plain type ailerons, F-K had Frise type ailerons, and all Spits - maybe post-war versions didn't? - had Frise.)

The only really good point is about roll inertia, the 109 indeed seem to have been praised for brisk aileron control (that means, quick response, not neccessarily the same as maximum rate of roll) at low to medium speeds. And of course the 109 benefited from its high-lift devices on the wing in numerous ways, but the main thing about the 109-p51 climb rate difference was obviously that the latter was about a ton heavier.

I noticed that, too (roll performance). To continue in this vein, as the speed of the 109 picked up during development and the initial roll response dropped off due to less aileron deflection per pound force (at the stick) the guns were removed from the wings (F model) to bring the initial roll response (not to be confused with sustained roll) back up. No further action was taken on addressing high speed roll performance until server tabs were developed for the K (et al) but not uniformly applied and as a rule disabled when installed.

Do you know who developed the servo tabs?

Last edited by zipper; 12-31-2011 at 03:58 AM.
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Old 12-31-2011, 12:59 PM
Kurfürst Kurfürst is offline
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IMHO the main thing that effect roll response is the change in wing shape and aileron layout. The wing of the 109A-E was different from the 109F-K, and so was aileron layout. As noted, A-E had plain type of ailerons, and it seems from accounts it was brisker than the F-K. This may be down to the shape/size of aileron and its placement, as after all, what the ailerons do is changing the lift on the wings (increasing on one wing, decresing on the other, hence the roll).

The F-K had Frise type ailerons, which by their nature help to reduce aileron forces (Frise type ailerons have their hinge point moved slightly backwards, and the leading edge of the aileron protounds when deflected into the airstream, which helps a bit.)

As for the Flettners tabs on ailerons, these primary found on photographic evidence mounted on WNF (Wiener-Neustadt, near Vienna, Austria) produced Bf 109G-6/14 and G-10. I have some docs relating to this, trials showed that the effect was that 2/3s aileron deflection was possible at at around Mach 0,70+. WNF did not produce 109K however, only Mtt Regensburg did. The K was supposed to have them, but its difficult to find pictures with them. Perhaps it was mounted, but there are too few pictures of Ks sadly. What the K had however was increased gear ratio on the elevator (elevator deflection was reduced), hence stick forces in pitch decreased.
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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
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  #9  
Old 12-29-2011, 02:47 PM
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That and the fact there aren't many viable airframes out there and the owners willing/able to test the real performances in the name of science. Some things are simply now passed to legend...
It is true that most of the warbirds around today are not in their original WWII configurations..

The good news is most WWII planes were tested and a lot of those test results still exist.. The bad news is not every field mod and or variant of a particular plane was re-tested..

The sim makers use these test results (outputs) as a sanity check of their FM.. That is to say the data from these test reports are not used as inputs to create the FM (unless your talking about a simple table based FM) just used as a check of the FM

Pretty simple, the FM results match the test data results or they don't.. So one would think that would be the end of the discussion, right?

Well sadly no

As noted you will be hard pressed to find test data for every variant of every plane in the game.. And even when you do find data for a particular variant in the game there will be people standing by to give it a thumbs up or a thumbs down.. For example, some will toss out the 'theory' that the Russian data was 'tweaked' to show the planes performed better than they actually did. The theory being they did that to keep uncle Joe from cutting off their heads.. Same argument is made with regards to some of the late war German data.. A similar argument is applied to US planes.. Especially with regards to test results from the manufacture.. The idea that the manufacture has tweak the results to show the plane performed better than they actually did to sell their plane.. Problem with that argument is USAAF also did acceptant testing that shows there was typically no tweaks made.. At least I have yet to see anyone post the results done by the manufacture that far exceeded what the USAAF was able to obtain.

Personally I tend to ignore all those who float those 'theories' especially the ones that will float the 'theory' for the planes they don't like and not even consider the possibility of the 'theory' for the planes they like (read hypocrites)

The only area of real world test data that I would consider to be suspect is that of the calculated/estimated type. That is to say data that was not from an actual flight test, just desk top calculated results based on what they expected to see if they actually did the test.. For example say they have a plane that they have already tested.. Than later figured out a way to increase the horse power.. Instead of re-doing the actually flight test, they would start with the flight test results from the previous test and simply increase the top speed and climb rate by an amount they 'calculated' it would increase by due to the increase in horse power. This is the kind of data that should be taken with a grain of salt imho, and on that note this is the kind of data the Germans did a lot of near the end of the war.

Long story short, even if you could find a WWII war plane with a WWII configuration and an owner willing to put it threw the paces of a test.. You will find someone who will try to find something wrong with the data.
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Old 12-29-2011, 04:16 PM
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Originally Posted by cheesehawk View Post
So true, and it seems the data we have from the war period doesn't cover everything we would think of now (i.e. roll rate progression, acceleration are some I've never seen referenced data on, although my research is mainly limited to what you can find on the internet),
True.. the standard acceptant testing consisted of a top speed per altitude test and a rate of climb test.. Which typically also produced a time to climb test.. Very few roll rate tests were done, and even fewer acceleration testing was done. It wasn't until just after the end of WWII that they switched to Ps testing for fighters

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and funny hand drawn graphs that aren't posted at the Imperial War Museum or the Bundeswehr Military History Museum, leaves too much room for suspicion on accuracy.
Ya lost me there.. ?

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Add to that the somewhat contradictory testimonies of the pilots, and no wonder we have wildly differing opinions on what each of our beloved aircraft should do.
Bingo!

I have an old saying.. For every Spitfire pilot that said he could easily out turn a Bf-109 there is a Bf-109 pilot that says he could easily out turn a Spitfire

Which only proves that combat reports by combat pilots are not something the FM results should be based on.. For many reasons, like they typically are one sided stories, typical preformed under none standard conditions, typically don't contain enough information to recreate the scenario..

In the end combat reports say more about the realitive pilot skills/luck than the planes performance
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