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Bf-109F-4 and a bleak time for RAF

Aviation Discuss Bf-109F-4 and a bleak time for RAF in the World War II - Aviation forums; Originally Posted by DerAdlerIstGelandet I am staying out of this arguement because I personally think that it is foolish to ...


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Old 12-18-2006, 12:38 PM   #76
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Originally Posted by DerAdlerIstGelandet View Post
I am staying out of this arguement because I personally think that it is foolish to argue over these 2 aircraft. They were well matched, each had its own advantages over the other and also had disadvantages over the other.

Having said that, they were both great aircraft.

Having said that, The guys who are biased toward the allied aircraft, do the same as you say about the guys biased to the German aircraft.
Seconded

Last edited by DerAdlerIstGelandet : 12-18-2006 at 12:41 PM.
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Old 12-18-2006, 12:44 PM   #77
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Sorry Glider I had to edit the smiley in my post as well as the smiley in your quote of mine.
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Old 12-18-2006, 01:48 PM   #78
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Last edited by Chingachgook : 01-30-2007 at 08:37 AM. Reason: piss poor grammer
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Old 12-18-2006, 01:50 PM   #79
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the -109 series and spits were in constant competition during the war, no aircraft had an advantage for more than a couple of months before some new mark or varient changed the balance so it's not until later in the war you can make general comments like that, by which point the spit is generally considdered the better combat aircraft..........
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Old 12-18-2006, 03:13 PM   #80
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Because the evidence shows that the Spit turned tighter does not change my belief.
It shows your narrowmindness, cause there's no such evidence.
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Old 12-18-2006, 03:38 PM   #81
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Last edited by Chingachgook : 01-30-2007 at 08:37 AM. Reason: piss poor spelling
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Old 12-18-2006, 03:50 PM   #82
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Slats have almost no effect on lift, their only real function is to increase critical aoa. They allow the 109 to pull higher coefficients of lift, but do not increase lift at a given cl.
Which is why the effect of slats are not shown in the Russian tests. The tested turns are all sustained turns, ie. mild, 2-2.5 G turns at best. Without the slats opening, the 109 is just a fairly high wingloading aircraft with corresponding turn performance. The slats won't deploy in these mild turns, they don't make their effect felt; they deploy in the high-G, hard turns. That's why the 109 is generally described to 'shine' in hard, high-G turns.

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The problem with that is induced drag is proportional to the square of the CL, so whilst the 109 can pull higher cl, it does so at the expense of far more drag than the Spitfire.

Quite simply, larger wings generate less induced drag.
Problem is, your little model misses a *slight* factor, that is that it's the wing that creates both drag and lift. An bigger wing also develops proportinally higher drag, it's not that it's just develops more lift without any extra drag.

To put it simply, the 109 has far less drag than the Spitfire. Yes, to obtain the same lift it needs higher AoA used, which increases drag greatly. But wheter the 109 has more drag at high AoA or it has still less drag when it has the same lift as the Spitfire, is something that needs to be worked out by calculation.

You've already posted the information I posted a while ago but you did it selectively:

Quote:
Originally Posted by Hop View Post
The Russians tested turn times for aircraft. Their figures, all at 1,000m altitude:

109F4 - 19.6 - 20.5 secs (at 2900 kg)

109G2 - 22.6 (at 3235kg) 20 - 21.5 secs (at 3023kg)

109G4 - 21 secs (at 3027kg)

Spitfire Vb - 18.8 secs (at 2920kg)

Spitfire LF IX - 18.5 (at 3351kg)
Let's see (added wingloading):

Bf 109G-2 : 20 secs* at 3023kg), using 1300 HP (187 kg/m2)
Spitfire LF IX - 18.5 at 3351kg, using 1690 HP (149 kg/m2)

Let's add Soviet fighters and see if your theory that wingloading is so important makes any sense...

Yak-3 - 17 seconds (2697 kg, 182 kg/m2) - 1290 HP
Yak-9 - 17 seconds (2870 kg, 167 kg/m2) -
Lagg3 - 18 seconds (2990 kg, 170 kg/m2)
La5FN - 19 secons (3290 kg, 188 kg/m2) - 1850 HP
La-7 - 18 secons (3315 kg, 189 kg/m2) - 1850 HP

* The Russians gave both left/right handed turns for the 109, turning to one side generally means better turn turn time because of torque. Wheter it's left or right depends on propeller rotation direction) It makes sense to use the optimal turn direction, as this was the case of the Spitfire as well.

Uh-oh. Something ain't right with your model.The Spitfire's big wings supposed to give 'much less drag', but then why do I see that with so much more power, the Spitifire actual turn times are not better and generally worser than the Soviet turn times.

Especially look at the Yak-3. This plane should be an awful turner, at least in Hop's world. It has a shitty engine with 400 HP less than the Merlin. It has the smallest wing area of the entire bunch and fairly high wingloading.

Ie.


Yak-3 - 17 seconds at 2697 kg, 182 kg/m2 - 1290 HP
Spitfire LF IX - 18.5 seconds at 3351kg, using 1690 HP (149 kg/m2)
Yet it convi

The Spitfire has 22.5 m2 wing area, the Yak much less 14.8 m2 wing area.

Explain please, how can it be that the Spitfire...

- with so much power : 1690 vs 1290
- with so much bigger wings : 22.5 m2 vs 14.8 m2
- with so much better wingloading : 149 kg/m2 vs. 189

...gets OUTTURNED by the Yak-3.

If we go by your model of how things work, the Spitfire should quite simply outturn the Yak-3, because it has much better wingloading, and if it has better wingloading, it is supposed to have less drag in turns, at least according to you. But it doesn't seem to work that way in real life...

What the Yak-3 DOES have however, is :

- extremely low drag
- extremely postive power-to-weight, power-to-drag ratio.



Quote:
The 109 can pull to higher AoA, possibly even generate enough lift to counteract the Spitfire's huge wing loading advantage, but it does so at the expense of enormous amounts of drag, which is why it can't turn as well as the Spitfire.
As noted, the Spitfire's huge wing loading advantage already means that it has far more drag to start with. The Spitfire's 'huge wing loading advantage' also comes with huge drag because those huge wings create huge amounts of drag as well.

Especially considering that the Spitfire's big wings are not very good at creating lift/area... the Spit wing has washout on a large area, which effectively means that much of the wing is developing less AoA and lift than the rest. The Spit's wing is also of the thinnest profile of all WW2 fighters which means it actually develops the least lift per wing area. It's not an efficient lift-creating device. It was built for speed as a matter of fact. 1930s designers were fixated on the fast monoplane fighter. The Brits were no exception.

The huge wing was never meant for turns by it's designers, the only reason for it was that they needed to fulfill the RAF's requirement of houseing 8 machineguns in the wings, and they needed space (depth) for it.

Last edited by Kurfürst : 12-18-2006 at 04:40 PM.
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Old 12-18-2006, 04:09 PM   #83
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Allright guys. A good debate is cool and all and everyone loves them and great information comes out of them, but lets not start insulting each other. There are better ways to get your point across.
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Old 12-18-2006, 04:29 PM   #84
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Originally Posted by Chingachgook View Post
Hehe. You are something.

3 different tests from 3 different countries. One of which just happend to be THE COUNTRY THAT BUILT THE PLANE! You are beyond reason perhaps? Tell me again how the German test pilots did not know how to fly their own planes...

Show me a test (German even) that shows a head to head test between a Spit and a 109 where the 109 out turns the Spit. Soren. Please.

I will even help you out here. I have heard that the Brits said (at some point) that the 109F2 that they tested could out turn the Vb above 18k at higher speeds (or 22k - I have heard different versions of the story). I have not seen the real doc but I would be willing to believe it based on powerloading at higher alts...

But for everyones amusement here is the portion of the German test again...

Before turning fights with the Bf 109 E type, it must be noted in every case, that all three foreign planes have significantly smaller turning circles and turning times.
An attack on the opponent as well as disengagement can only be accomplished on the basis of existing superiority in performance.



From : Kr.-Fernschr.Ob.d.L.,Führ.Stab Ia Nr.8092/40 g.K. (II)
(only to Lfl.3)


Subject : Comparison flight between Bf 109 E, Bf 110 C, Spitfire, Hurricane and
Curtiss.
Keep running circles Chinny.

The test you so love to refer to is as explained not valid as it involves the 109E which is known to have issues with its slats, plus most pilots at that point didn't dare push past the deployment of the slats. The exact same goes for the British tests, where the British test-pilots aborted any maneuver as soon as the slats deployed.

As to the Russian tests, well what Kurfürst said.

Now perhaps you'd be so kind as to back up your claim in aerodynamic terms ??
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Old 12-18-2006, 04:42 PM   #85
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I don't know a lot about these two aircraft, but I suspect if these two planes were swapped and the Germans flew the spitfire and the British flew the Bf-109, there would have been no discernable difference in the war, or loss rate, or anything. That's how close I think they are technically. As DerAlder said, both were great aircraft. They were flown by brave and capable men, each motivated by a desire of protecting their homeland.
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Old 12-18-2006, 08:48 PM   #86
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Last edited by Chingachgook : 01-30-2007 at 08:38 AM.
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Old 12-18-2006, 09:25 PM   #87
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Originally Posted by Chingachgook View Post
Soren, your aerodynamic terms somehow do not pan out in any real tests done by anyone or in the combat reports (109s falling out of the sky trying to stay in turns with Spits etc - as reported by German pilots). You have to make an excuse for all of the facts. When you resort to conjecture and equivocation there is simply nothing left to say.
Just today I was reading a report by a 47 pilot Hubert Zemke (also flew 38s and 51s) regarding the 109's sharply degraded performance at altitude - pilot said inexperienced 109 pilots would at times inadvertently get themselves into a spin, while other pilots would split-S and dive for denser air. 47s would pounce down upon them acheiving strong advantage w/ their excellent diving performance.
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Old 12-19-2006, 05:39 AM   #88
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Just today I was reading a report by a 47 pilot Hubert Zemke (also flew 38s and 51s) regarding the 109's sharply degraded performance at altitude - pilot said inexperienced 109 pilots would at times inadvertently get themselves into a spin, while other pilots would split-S and dive for denser air. 47s would pounce down upon them acheiving strong advantage w/ their excellent diving performance.
I was reading some Pilot encounter reports from P-47 FGs from late 1943. They reported the same, the P-47 would outdive, outturn and outclimb the Me 109 at those high altitudes.

The Me 209s (an later version of the Me 109 I presume ) they encountered however, did outdive, outturn and outclimb their P-47s with ease.
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Old 12-19-2006, 05:46 AM   #89
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Originally Posted by Chingachgook View Post
Soren, your aerodynamic terms somehow do not pan out in any real tests done by anyone or in the combat reports (109s falling out of the sky trying to stay in turns with Spits etc - as reported by German pilots). You have to make an excuse for all of the facts. When you resort to conjecture and equivocation there is simply nothing left to say.
Unfortunately my perception is that you are describing your own attitude here. You make vogue references to 'real tests' and '109s falling out of the sky reported by German pilots'. That's all fine but there are plenty of such accounts available from both sides, they prove little apart from that the opposing pilot's experience and the initial tactical and energy situation were major factors in manouvering fights.

A while you claim Soren is 'making an excuse' to your voguely references and massively generalized 'facts', you on the other hand simply close your eyes and ignore the accounts Soren has posted. Ie.


Walter Wolfrum, German fighter ace. 137 victories.
"Unexperienced pilots hesitated to turn tight, bacause the plane shook violently when the slats deployed. I realised, though, that because of the slats the plane's stalling characteristics were much better than in comparable Allied planes that I got to fly. Even though you may doubt it, I knew the Bf109 could manouver better in turnfight than LaGG, Yak or even Spitfire."

Herbert Kaiser, German fighter ace. 68 victories.
"Personally, I met RAF over Dunkirk. During this battle not a single Spitfire or Hurricane turned tighter than my plane. I found that the Bf 109 E was faster, possessed a higher rate of climb, but was somewhat less manouverable than the RAF fighters. Nevertheless, during the campaign, no Spitfire or Hurricane ever turned inside my plane, and after the war the RAF admitted the loss of 450 Hurricanes and Spitfires during the Battle of France." In the desert there were only a few Spitfires, and we were afraid of those because of their reputation from the Battle of Britain. But after we shot a couple of them down, our confusion was gone."

Erwin Leykauf, German fighter pilot, 33 victories.
"During what was later called the 'Battle of Britain', we flew the Messerschmitt Bf109E. The essential difference from the Spitfire Mark I flown at that time by the RAF was that the Spitfire was less manoeuvrable in the rolling plane. With its shorter wings (2 metres less wingspan) and its square-tipped wings, the Bf 109 was more manoeuvrable and slightly faster. (It is of interest that the English later on clipped the wings of the Spitfire.)
For us, the more experienced pilots, real manoeuvring only started when the slats were out. For this reason it is possible to find pilots from that period (1940) who will tell you that the Spitfire turned better than the Bf 109. That is not true. I myself had many dogfights with Spitfires and I could always out-turn them. This is how I shot down six of them."


Pierre Clostermann, Spitfire pilot.
"I tried to fire on a '109' that I spotted in the chaos. Not possible, I couldn't get the correct angle. My plane juddered on the edge of a stall. It was comforting that the Spitfire turned better than the '109'! Certainly at high speed - but not at low speed."


Judging from pilot accounts, the 109 would always outturn a Spitfire and emerge as a victor, and the Spitfire would always outturn a 109 and emerge as a victor.

Oddly enough, there are few accounts from pilots describing how they were outturned and shot down from either side. I presume that has to do something with the conseqences. Dead pilots are horrible story-tellers.
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Old 12-19-2006, 07:12 AM   #90
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Adolf Galland in a conversation with Goring in August 1940 was able to turn tighter than the 109

Heinz Knoke wrote of the Spitfires 'The bastards can make such infernally tight turns there seems to be no way of nailing them'.

The War Diary of I/JG 3 for August 31st 1940 states that the Spitfires turn very well at higher altitudes and tighter than the 109.

Gunther Rall wrote that the Spitfire had great lift and was very manoeverable and he couldn't catch them in a climb. In contrast he wrote that he didn't like the slats on the 109 and found the cockpit narrow compared to the Spitfire.

In short gentlemen for every quote you can find praising one aircraft, you will find another praising the other.

IE THEY WERE A FAIR MATCH
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