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It was rather different Packard Merlin. A two speed supercharger WITHOUT a SECOND STAGE and WITHOUT INTER-COOLER as used in the P-51B-D.What i find interesting about the MTO is that the P-40F was used, featuring the Packard Merlin found in the P-51D.
The P-40s had a ceiling of 29,000ft but probably could only function decently as a fighter below 20,000ft.
It was rather different Packard Merlin. A two speed supercharger WITHOUT a SECOND STAGE and WITHOUT INTER-COOLER as used in the P-51B-D.
The "ceiling" or service ceiling of most planes was the altitude at which the climb rate dropped to100ft per minute. This is also an indication of the excess power available after level flight is achieved. Please note that "Climbing speed" is where this excess power is available. not max level speed.
MAX. ceiling is the altitude at which the plane cannot climb anymore and Max speed is the same as stall speed which also means the airplane cannot turn or maneuver as the extra drag will cause the airplane to stall.
An airplane with a service ceiling just a few thousand feet higher than another aircraft might, at an altitude a few thousand feet below plane "B"s service ceiling have double the rate of climb, a much better ability to either maintain speed or height in a turn.
The P-40 F might be able to effectively fight 3-5000ft higher than a P-40E but that does not mean it can fight at the same altitudes (24,000-30,000ft) as some Spitfires and the 109s.
No surprises I'm afraidI'd be surprised to see how the Merlin Mustang and P-40F match up in level speed at 15,000ft
good read, need to take in consideration the him talking of training biplace Yak 7
No surprises I'm afraid
P-40F around 352mph @ 15,000ft
P-51B around 415mph @ 15,000ft
=Vincenzo;631381]specifically he tell that in training never flew alone in yakovlev, late he never talking to fly with yakovlev.
why looking a enemy test or a special purpouse test when there are the official flight trials available?
Well, i can't look at a test in 43 to see how a fighter performed in 42.
Even flight trials are done to measure an increase in performance, and aren't always best for comparison reasons, but that is all we have short of actually flying the planes ourselves.
And noteably, there are flaws in the data of most tests which have to do with limitations in instrumentation. For that reason i mention a margin of error +/- 10mph (16kph).
Nothing i'm saying is doctrine, simply my educated opinion.
Even with this said, production variant 109s tested and rated in early 43 would not have seen combat til mid 43/late 43. And by then the P-40 was being phased out with P-47s and P-51Bs.
Its not really a relative discussion of speed in this context, simply put, the 109 was faster, however speed advantage was reduced with altitude.
BTW, the speed at 15,000ft by the P-40F of 352mph, was achieved at 48" of boost. It was ran in combat up to 55" and according to some pilots could achieve over 60" of boost in emergencies.
Australian pilots reported pushing 70"s of boost using their Allison driven Kittyhawks. (P-40E) with out problems, yet you see more published numbers on speed indicated when they were used at 42" of boost.
http://www.raafwarbirds.org.au/targetvraaf/p40_archive/pdfs/Allison 1710-39 abuse.pdf
You can see how much power the Allison was capable at lower altitudes where supercharging was not such an issue as it was in thinner atmosphere. The horsepower is considerably higher.
The Merlin was better at altitudes of 10-15k ft, where i have to wonder what speeds could be produced using higher boost pressures.
Perils P40 Archive Data
So speed and advantage is a bit difficult to nail down with discussion of test flights alone,
Bill
and why compare a 42 gustav neither P-40F or P-51B fightning in '42?
i've laready reading in this forum info on overboosted P-40 but (i still not read the links) i think this give best a lower altitude (lower of 15'k)
Official specifications for Bf 109G-1(as well as -2/-3/-4):
Kurfrst - Mtt. AG. Datenblatt, Me 109 G - 1. Ausfhrung
Range figures for Bf 109F/G:
Interesting graphic.
Has the Spitfire IX fast cruise speed at almost 365mph (no external fuel tank) while the 109G's fast cruise speed is approx. 300mph.
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I've been looking for those. Do you have figures on the 109Fs specifically the R types used as long range fighters? Possibly even early Gs or G-2s? These look to be late war figures.
The following comes from a British report on a captured Bf 109G-2/trop in North Africa (same plane today flies restored as Black Six)
Kurfrst - Bf 109G/trop Middle East trials: Dimesnions, Weights and Performance
Later the British intel issued revised range figures, reduced to the ca 600/1000 miles as seen on the first range doc I posted, but there is no specific reason why the figures were revised, and it only seem to effect range at economic cruise).
If you mean 109Fs with drop tank under "specifically the R types", it wasn't a seperate variant, nor is, for example, a designation like "F-4/R3" correct, there wasn't a suffix when a drop tank was carried (it could be carried by all). Only special variants had such designation, like the F-4/Z (GM-1 boost) or the F-4/R1 (gondola cannons, but only because only these late Fs could carry gondolas, there was no such on the G-series, as all were prepeared to do so).
As for the 109Fs range, German papers give it as roughly the same as the G-series, ie. the 109F-4 is given is German datasheets and range tables as with a range of 1600 km with droptank, 835 km without, at a cruise of 410 km/h.