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I do apologize as I meant no personal offense, the image just struck me as very odd.All I can say is that it's a photograph that I took at the NA of an original paper. Original doc's in the NA are often blurred as they were typed and to produce multiple copies the process produced the blurred effect. People often would write on their blurred original and that of course would be sharp.
Showing my age I can remember using carbon copies and duplicating machines at work..
If you wish I could post other examples of doc's with similar characteristics
54 in is take-off power, but 48 in was the military power at 3000rpm and 44in at 2850 rpm was the max continous rating.
65inches would be just about 18lbs of boost. Not sure when that was approved (if ever) as opposed to a 14-16lb rating. For most of 1942 there was no official WEP rating and boost was limited to 9lbs after take-off. 1943 is a different story.
Comparing that level of boost to the Typhoons engine running at max continous is bogus.
Even an early Typhoon in combat would use 1-2 pounds more boost and several hundred more rpm than the power level used for the climb rate you posted. Later Typhoons used an additional 2lbs of boost and another 150rpm at full power.
Also from the wherever its worth desk, just because people have different sets of performance stats on an aircraft doesn't mean that EITHER of them is cherry picking information. God knows there is oceans of conflicting information on most planes.
I've always tried to look at different aircraft with a dispassionate eye as far as performance even though I do have my favorites but still much of the info I have gleaned from what I have read over the years turned out to baloney. And who knows maybe much of what I believe now will turn out to be bogus in the future.
That is kind of the point of this forum after all. Or at least one of the points is to get to the bottom of things and well all be better off for it.
Just my 2 cents.
In the Summer of 1942 the Sabre engine in the typhoon was rated at 3500rpm and 6lbs boost for 30 minutes. That was the power level used for climbing tests. Full power was 3700rpm and 7lbs of boost.
By the summer of 1943 they were testing and approving 3700rpm and 9lbs of boost for combat.
Low altitude climb for the Tiffy using those throttle settings was about 3800fpm. And it could reach 20,000ft in 7 minutes. This for an approved level of power. Not what a particular squadron or pilot/ crew chief did. Granted the Sabre engine was not particularly tolerate of abuse or tinkering by squadron mechanics.
While Merlin XX series engines did finally get approved for 18lbs of boost (65-66in) it took a while as I believe the supercharger drive system had to be beefed up to handle the increased load.
Edit. The Sabre IIB engine used in late Tempests and the last 500-600 Typhoons (late 1944 and 1945 production) were rated at 3850 rpm and 12 pounds boost but this is well after the time period in question.
There were Sabre II engines, Sabre IIa engines and Sabre IIb engines, Some Typhoons were built with one and then re-engined with another and some IIas could converted to IIb standard with a strengthened reduction gear and a modified boost control. But this would be 1944 or later.
No apology needed,we're spoilt these days.I do apologize as I meant no personal offense, the image just struck me as very odd.
Perhaps dealing with documents more from the digital age in recent years, I've become accustumed to the exact formatting and have forgotten about how documents could vary from typewriter to typewriter, or documents that came off a teletype could be a bit off...and yes, the old "Ditto" machines with their purple or blue-black text along with the unique smell that permeated the paper for days on end.
And using Carbon paper was a joy especially if the forms were triplicate (or more), where you had to nearly do bench-presses to ensure the writing tranferred across all copies.
Again, my apologies
On the subject of turning.
Wing loading is an important indicator.
However it is not the only thing going on.
Unless somebody can explain how the Typhoon, with its higher wing loading has a slower stall speed?
I am not claiming the Typhoon can out turn the P-40 but the difference between them might not be as bad as the wing loading alone would suggest.
Now for sustained turning, each airplane has a combination of speeds and turn radius it can sustain over long periods of time while neither losing speed or altitude. Some planes can turn much harder (smaller radius) but only at the cost of bleeding off speed until the plane stalls or by doing a spiraling decending turn.
Planes with higher climb rates usually have more power/energy to fight this speed loss without having to lose altitude.
I would note that a Spitfire I might have lucky to sustain a 3 g turn at 10,000 ft without losing altitude and that is at speed well under 300mph.
We all know that a Spit mkI can turn much tighter than 3 Gs. It just can't do it at high speed or without losing altitude.
The 109E happened to be worse.
Hope that explains things.
Two words - Joachim Marseilles......he flew a 109 and shot down quite a few P-40s.
Things started to improve when tropicalised Spitfires arrived to escort the P-40s.Scoreboard here. I gave up after counting 32 P-40 kills. Interesting that on three consecutive days he shot down 4 of them. He also shot down a whack of Hurricanes. I can't verify the accuracy of the article, it was posted late November 2014. Hans-Joachim Marseille
Scoreboard here. I gave up after counting 32 P-40 kills. Interesting that on three consecutive days he shot down 4 of them. He also shot down a whack of Hurricanes. I can't verify the accuracy of the article, it was posted late November 2014. Hans-Joachim Marseille