Originally posted by GScholz
It's not a match for any of its contemporary Allied or German fighters. They are far superior in everything but range and in some cases manoeuvrability.
Originally posted by HoHun
Hi Flakbait,
Well, in fact the debate is somewhat academic as both radial and inline engines finally evolved into quite similar three-dimensional engines, so they both have to be considered interim types :-) Note that V engines aren't strictly inline, anyway, nor are twin-row radials strictly radial.
The point about the A6M's radial is simply that it has about the same power as the DB601A, and less than the Merlin III, while being an air-cooled radial with a big drag penalty compared to a liquid-cooled V engine of the same output.
Regards,
Henning (HoHun)
Originally posted by HoHun
Hi Flakbait,
>And it is a rather moot point regarding the A6M engine being radial since it hit nearly the same speeds as some of the hot-water, 12 cylinder engines with slightly higher HP ratings.
Actually, it didn't even come close:
Spitfire I: 571 km/h @ 5000 m, 487 km/h @ sea level
Me 109E-4: 584 km/h @ 5000 m, 480 km/h @ sea level
A6M2: 524 km/h @ 4880 m, 434 km/h @ sea level
Quite obviously, the higher drag of the radial engine was at least partially responsible for that.
Regards,
Henning (HoHun) [/B]
Originally posted by Karnak
For example I recall reading that the He219 never broke 400mph level flight in service despite the official speed being 416mph.
Originally posted by F4UDOA
Karnak,
I think there are two factors contributing to the disparity of performance between the KI-84 and P-51H.
1. An overstatement of performance of the P-51H.
2. The high octane fuel use by the AAF in the testing of the Ki-84.
The truth lies somewhere in between.
Originally posted by F4UDOA
JoeB.
I didn't realize your were a Philly guy.
I am in Cherry Hill now, Grew up around George Washington High.
Or maybe we talked about this already and I forgot.
Anyway
Go Birds!
The A7M1 prototype flew for the first time on May 6, 1944, test pilot Eisaku Shibamaya being at the controls. Test pilots reported that the A7M1 handled extremely well, and that the use of the combat flaps made the A7M1 just as maneuverable as the Zero. However, they also reported that the aircraft was significantly underpowered for its weight. The Homare 22 delivered only 1300 hp at 19,685 against a calculated rating of 1700 hp, and at this altitude maximum speed was only about 350 mph. In retrospect, Horikoshi was right. Because of its disappointing high-altitude performance, on July 30, 1944 the Navy ordered that further work on the A7M1 be suspended after the second prototype had been built.
Originally posted by flakbait
.... An easy way to check the speed differential between fuels would be to take a look at test reports of a given aircraft using different octane rated fuels. If the F4U was tested with 87, 110 and 120 octane fuels a quick comparison between top speeds would let anyone see how much speed is gained from using a given type of fuel.
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Flakbait [Delta6]
(http://www.wa-net.com/~delta6/sig/veggie.gif)
Originally posted by joeblogs
Yes, we are pretty darn close.
-Blogs
Actually the reason I asked was so we could try to reverse-calculate the Ki-84 speed. If the TAIC test used 120 octane fuel, and the Hayate normally used 92, maybe another aircraft has a set of numbers from two different fuels. Granted it wouldn't be perfect, or exact, but it would be a rough guess as far as the actual top speed. Hence my example of the F4U; if it had numbers from two different fuels, the speed difference could be used to roughly SWAG the Ki-84 speed difference between the TAIC test and the actual top speed.
Originally posted by F4UDOA
Actually Flakbait that is really easy to do without the use of different fuels. Since the use of higher octance fuel only allowed for increased power by incresed allowable manifold pressure you can look at the F4U at three differrent MAP's, Normal, Mil and Combat powers.
What was the highest MAP the KI-84 could run at on 92 octane fuel? What did MAP did it use at 120 octane? If you know the differance there you can apply that to the F4U-1D.
At 60"MAP at sea level it could reach 358MPH (With pylons attached). At 44" MAP (normal power) it could only reach 320MPH. There is 48MPH difference on 16" of MAP. Granted that is also a difference between 1675HP and 2250HP.
If you know the difference in MAP with the KI-84 you should get an idea of the HP gain with higher octane fuel. Based on the F4U-1D I would say the difference is very significant. Enough to account for 30MPH at least.
Originally posted by Angus
I tend to disagree with this point.
From the Merlin 61 onwards for almost 2 years, the Germans were indeed completely inferior in the very high altitude department.
Originally posted by F4UDOA
Flakbait,
I wasn't comparing the two.
Just showing that the difference on the F4U-1D from 44"MAP to 60 " MAP is 38MPH.
It doesn't matter if the KI-84 is using 92 octane or 120 octane fuel unless you are at maximum MAP. At normal power in any aircraft the fuel octane will not affect performance to any great degree and less than max power. Octane only affects performance at max power by preventing premature detonation and allowing for higher MAP. An F4U with 100 octane fuel is just as fast as one with 120 octane fuel at normal or mil power.
So if you look at the HP increase in the F4U from 44" to 60" you can see it increases HP from 1675HP to 2250HP and increase of almost 35%. If you know what MAP the KI-84 was running at 120 octane then you can reverse engineer the HP and probable speed increase.
Originally posted by flakbait
Ahhh, okay, now I see how its done. Now to track down a copy of that rotten report and see if they list the MAP it was pulling.
Thanks DOA!
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Flakbait [Delta6]
(http://www.wa-net.com/~delta6/sig/end_net.gif)
Originally posted by Karnak[/B]
Barbi,
Erm, which German high altitude fighters are you refering to? I've never heard of any in 1942. The first I know of is the Ta152, and yes, that one is a doozy.
[/B]
However I know of nothing in 1942 that matches the Merlin 61 Spitfire F.Mk IX,
[/B]
or in 1943 that matches the Merlin 70 Spitfire HF.Mk IX,
or anything in 1944 that matches the Griffon 65 Spitfire F.Mk XIV.[/B]
There is a reason the British built the Merlin 66 Spitfire LF.Mk IX and it was because the critical altitude of the German fighters was all in the medium altitude ranges and the Merlin 61 was too high. [/B]
Originally posted by Angus
Hai, F4UDOA-san.
Originally posted by Angus
LOL :D
Anyway, some information from a 190 thread that might come in handy.
Crumpp pointed out that the Germans were ahead of anybody else in high quality paint. That influences top speed some little bit.
I wonder how those matters were by the japanese.