Author Topic: Why are the Japanese planes so slow?  (Read 2839 times)

Offline MiloMorai

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Why are the Japanese planes so slow?
« Reply #45 on: November 10, 2004, 07:28:31 AM »
flakbait,

 can you explain what you mean by 'inclination of piston angle'?

Offline F4UDOA

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Why are the Japanese planes so slow?
« Reply #46 on: November 10, 2004, 08:17:09 AM »
Quote
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.


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.

Offline flakbait

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Why are the Japanese planes so slow?
« Reply #47 on: November 10, 2004, 09:35:47 AM »
Quote
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.


DOA, reverse it. I didn't mean to say that I wanted to compare the Ki-84 to the F4U, I wanted to compare the speed difference of the F4U using different fuels to the Ki-84 performance in the TAIC test. Unfortunately, I can't find a copy of the TAIC report to get the MAP numbers they used. What's worse, you can't use the MAP and HP difference between standard running pressures (MIL, normal, cruise) with 92Oc fuel to figure a MAP and HP rise on a higher octane fuel. The numbers would be entirely different on 110Oc than 92Oc, with a different spread. So reverse-engineering the numbers from 110Oc (TAIC test) to 92Oc (Japanese gas) is nigh on impossible. Unless of course I'm way off and the MAP numbers simply rise in lock-step from one octane to another.

We know the Ki-84 in AH pulls +250mm (38.92"Hg) and puts out 1,800hp at takeoff. But Busa and several others have mentioned +350mm (42.92"Hg) for the pre-production machines as the MAP limit. Why this odd 4"Hg difference? Limiting an engine by 4"Hg doesn't make any sense, unless a different gearing for the super or another carb was used.

Ok, now I know what Kweassa felt like when trying to fathom prop problems. Brb, need Tylenol!


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Offline F4UDOA

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Why are the Japanese planes so slow?
« Reply #48 on: November 10, 2004, 12:30:11 PM »
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.

Offline VO101_Isegrim

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Why are the Japanese planes so slow?
« Reply #49 on: November 10, 2004, 01:39:44 PM »
Quote
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.


Hardly. They had GM-1 in the first place, against which the two staged Merlins didnt stand a chance... German high alt fighters were exceeding 700 km/h in 1942, no Merlin engined Spitfire came even close to that. Thats the techspec part.... production is another matter. The British could never produce high alt fighters in any serious quantity, they always came too late, too few. For every high altitude Merlin 61 engined fighter of the RAF, the Luftwaffe fielded TEN high alt fighters with equal or better performance... so you are wrong both technically and factually.

Offline Karnak

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Why are the Japanese planes so slow?
« Reply #50 on: November 10, 2004, 01:47:44 PM »
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.

However I know of nothing in 1942 that matches the Merlin 61 Spitfire F.Mk IX, 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.

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.
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Offline flakbait

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Why are the Japanese planes so slow?
« Reply #51 on: November 10, 2004, 01:56:48 PM »
Quote
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.



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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Offline joeblogs

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« Reply #52 on: November 10, 2004, 02:19:22 PM »
One thing to note about this comparison - its should favor the Japanese plane.

Why? Because you'll be reading off the performance curve of the Japanese plane at or near its highest output. Of course the designers configure the plane taking into account the performance of the engine.

For the American plane, however, you would be reading off the performance curve well away from the full potential of the engine. As a result you will be inferring something about speeds for a bigger and heavier plane that was designed to be bigger and heavier because its engine had much more top end power.

-Blogs

Quote
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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Offline Kurfürst

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Why are the Japanese planes so slow?
« Reply #53 on: November 10, 2004, 02:29:41 PM »
Quote
Originally posted by Karnak
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]

Karki,

so then you probably didnt hear about the Bf 109F-4/Z or the Bf 109G-1. The 109E-7/Z existed before that as well. And to leave the Germans, there was the Soviet MiG-3, too.


Quote

However I know of nothing in 1942 that matches the Merlin 61 Spitfire F.Mk IX,
[/B]

Hmm, actually the 109F-4 was faster, the 109G-1 was MUCH faster (over 700 km/h), the G-2/G-4 w/o any intercooler, any two stage cooler or other gimnick was just as fast. Not to mention, it was ten times as numerous in service...



Quote

or in 1943 that matches the Merlin 70 Spitfire HF.Mk IX,
[/B]

Again, 109F-4/Z, G-1, G-3, G-5, G-6/U2 etc. In fact the standard G-2 and G-4 wasnt that much off, maybe the HF Spit was some 10 km/h faster at altitude. And I mean the Spit HF IX, specially tuned for high alt performance, supposed to be the BEST high alt Spit at the time, which a mere 400 were built during the whole war, so I guess during 1943 maybe a dozen were built, pitted against the most ordinary fighter types the LW had.. WOW.

So in 42/43 the LW had thousends of 109Gs built/in service with very good high alt performance, the RAF had a handful of Mk IXs with about as good high alt performance, and 90% of the RAF was flying MkVs with waaaaaaaay inferior altitude performance to either the 109F or 109G..

I guess it wasnt the Jagdgruppes then that were concerned about finally getting some fighter with a comparable altitude performance to that of the enemy.. personally, I wouldnt be happy to meet a 109G at 8000m in a Spit MkV. Unfurtunately for me, chances are 9 to 1 that I will, I am flying in RAF colours in 1942, and for most of 1943.



Quote
or anything in 1944 that matches the Griffon 65 Spitfire F.Mk XIV.
[/B]

Hmm, Bf 109 G-5/U2/AS. :D If you include 1945 as well, I could say K-4s with the Doppellader, but even the rest of the AS or D engined 109s were quite close to it - and far, far more numerous, some 6500 being built. But frankly I doubt the Germans ever knew what a Spit XIV was, or that it even exists. I doubt that many British pilots knew. Again too late, too few. A mere five squadrons flying it, equivalent of single LW Gruppe... on the other side, the LW had very large number of high altitude 109s in service, which were again much faster at altitude than the common MkIXs of the RAF. Ironically, the LW had more Me 262 in the units than as many Mk XIV units the RAF had.. so I guess the LW had no real reason to be concerned about the high alt performance of it`s fighters... they had some allergic reactions, though, namely the Ta-152s, a fighter designed for a threat that never existed, but in the process it become a lot more than what was needed. Or what could be handled by the opposition`s HA fighters..



Quote

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]


There is much truth in that. The RAF developed the Mk IXF, with a much heavier and more complex engine and shorter range than the previous models, other parameters being sacrificed for good high alt performance. That was the first time they come up with something that could be compared to the German fighters in altitude performance. Then in 1943 they found out such rated altitude isnt required at all, there is no common operational use for it, there are no enemy flights at that altitude, and without a pressurized cocpit, the planes themselves are not fit for operating at such altitudes.. so they reverted back to medium altitude fighters, the LF Spits... the LW also toyed with two staged engines with intercoolers at the same time for the 109 (and you dont want to compare the Merlin 61 to the DB 628), and found out that the neccesary bulk and weight of the intercooler eats up most of the performance gain, its impractical most of the time, and for such specialized task, the optional GM-1 is a much more practical solution. Most fighters could compare with the best (and rare) types the enemy had, without maintaince and other problems, could be produced and sent to the front quickly and i quantities, and when really high performance was required, there were the high alt, GM-1 wielding units that simply dwarfed other high alt fighters. I find the German approach a lot more practical. And in 1944, they could improve the existing fighters very simply by adding a larger supercharger to the side of the existing engine, the /AS types were little more than that, really.
« Last Edit: November 10, 2004, 02:36:10 PM by Kurfürst »
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Offline Angus

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Why are the Japanese planes so slow?
« Reply #54 on: November 10, 2004, 02:49:00 PM »
Oh, dear, Izzy at it again.

"Hmm, actually the 109F-4 was faster, the 109G-1 was MUCH faster (over 700 km/h), the G-2/G-4 w/o any intercooler, any two stage cooler or other gimnick was just as fast. Not to mention, it was ten times as numerous in service... "

At what altitides Izzy?
And where do you have these numbers from. Have NEVER seen them before.
So you're basically saying that the DB was so uber that it performed as well at (the same?) ceiling alt without any other aid such as second stage and so? And for your info, the intercooler was a necessary thing to cool the air between the two superchargers, but intercoolers also have the effect to increase power as a positive, and it's relatively simple.
Typical for lorries and tractors today is the beautiful combo Turbo-intercooler.

A question: How many were there of these 109G-1's. Interested, cos I never heard them mentioned before.
Could they cruise at 43K like the Merlin61 Spit IX, in battle formation, and were they in wing strengths like them?

Now bring some stuff for the dinnerplate Plz....
It was very interesting to carry out the flight trials at Rechlin with the Spitfire and the Hurricane. Both types are very simple to fly compared to our aircraft, and childishly easy to take-off and land. (Werner Mölders)

Offline F4UDOA

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Why are the Japanese planes so slow?
« Reply #55 on: November 10, 2004, 03:06:29 PM »
Achtung Luftwabbles,

This is a Japanese Army KI-84 thread. Go beat your weinershnitzle somewhere else.:rolleyes:

Offline Angus

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Why are the Japanese planes so slow?
« Reply #56 on: November 10, 2004, 03:12:13 PM »
Hai, F4UDOA-san.
It was very interesting to carry out the flight trials at Rechlin with the Spitfire and the Hurricane. Both types are very simple to fly compared to our aircraft, and childishly easy to take-off and land. (Werner Mölders)

Offline StarOfAfrica2

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Why are the Japanese planes so slow?
« Reply #57 on: November 10, 2004, 04:21:54 PM »
I think that perhaps with all the technical information at our fingertips these days, even from as far back as 1940, maybe you gentlemen have overlooked a very important aspect of Japanese airplane development just before and during WWII.  Viewpoint.  

Japanese pilots (at least the IJN ones) came from a very small group of applicants.  Driven and determined to succeed, carefully screened and then put through some of the most rigorous and hellish training anyone can imagine, they were not just pilots.  They were warriors, in the truest sense of the word.  They were not just taught to fly, but to fight.  Their hand/eye  coordination was honed to a razor's edge and they were trained to develop their eyesight and sense of balance to almost superhuman heights.  They built very much on the Samurai traditions in the training of the IJN pilots.  Any combat, even in the air, was a 1 on 1 battle for supremacy.  Success, or the lack of it, was considered a direct reflection on the skill of the pilot.  The zero was carefully crafted and designed to suit this type of pilot, and was an incredible leap from the Claude fighters they replaced.  Speed was never consided of more than passing interest until long after they started getting their butts waxed later in the war.  Range, maneuverability, weaponry.  The plane was an extension of the individual to allow him to kill his enemy in the air.  

Even later planes like the Shiden and Hayate were not as fast as they could have been.  They compromised.  Tried to find a balance between what they felt a fighter was all about, and what the Americans did so effectively.  

Just my .02

Offline HoHun

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Why are the Japanese planes so slow?
« Reply #58 on: November 10, 2004, 04:48:20 PM »
Hi Star,

Interesting perspective, well written post, but after a thorough analysis, I've reached the conclusion that the facts don't bear it out.

The Japanese always pushed for performance, perhaps with an unusual emphasize on range, and while they valued manoeuvrability high, this didn't influence their designs much. It heavily influenced their pilots' comments, but that's deceptive.

The good manoeuvrability is mostly a byproduct of the low weight which was necessary to get the best performance out of the low-powered engines. Low weight was especially important to get decent high-altitude performance from inferior engine power. It also resulted from the emphasize on range as the high fuel fraction of their designs meant a relatively low combat weight when a good portion of that fuel was already used up.

Regards,

Henning (HoHun)

Offline StarOfAfrica2

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Why are the Japanese planes so slow?
« Reply #59 on: November 10, 2004, 07:22:34 PM »
I suppose it should also be considered that the original design specs for the A6M Zero-sen were submitted in 1937 when the A5M had just entered service.  This is what the IJN asked for in a fighter (which the A6M exceeded in all but one category by the prototype).

1. Maximum speed of 270 kt @ 4,000 m.
2. Climbing speed of 3,000 m in 9 min 30 sec.
3. Endurance of 1.5 to 2 hours at normal rated power.
4. Endurance of 6 to 8 hours at economical speed with drop tanks.
5. Armament of two 20 mm cannon and two 7.7 mm machine guns.
6. Provisions for two 60 kg bombs.
7. Provision for full radio and direction finder.
8. Takeoff run less than 70 m with a 27 knot headwind.
9. Maneuverability at least equal to the A5M.

The only failing of the A6M from this list was that it did not reach required top speed (cannot find top speed of the A6M1 prototype).  I have also read in accounts from two pilots (one would be the book "Samurai!" by Saburo Sakai, the other was an article I read in Warbirds but I cant find the issue right now) that the Zero did not have radios installed during service in WWII, and that is listed as one of the requirements.  


*The Navy ordered two prototypes and plans were submitted by Nakajima and Mitsubishi. Nakajima elected to drop their proposal for a fighter design and Mitsubishi submitted their design led by designer Jiro Horikoshi. The Mitsubishi prototype was the A6M1, retractable gear, all metal, low-wing monoplane, powered with a 780 hp Mitsubishi Zuisei 13 engine. During flight testing, the two-bladed prop variable-pitch propeller was replaced with a three-bladed variable pitch propeller. Apart from maximum speed, all requirements were met or exceeded. The Navy had authorized the production of an initial batch of A6M2s and military trials progressed rapidly. While flight testing the A6M1, a new power plant passed its Navy acceptance tests, and the 925 hp Nakajima NK1C Sakae 12, which was slightly larger than the Zuisei, was installed in the third A6M2 prototype. The initial trials were completed in July 1940 and the navy assigned fifteen A6M2s to combat trials in China. In China the A6M2s, reinforced with a number of production aircraft, destroyed 99 Chinese aircraft with a loss of only two of their own. The aircraft was accepted for production on July 1940 as Navy Type 0 Carrier Fighter Model 11 and in September 1941 were prepared for the impending war with the Allies. Modifications were introduced during production and A6M2 rear spar was reinforced and manually folding wingtips were incorporated to allow clearance on the carriers deck elevators. The modified aircraft was designated Navy Type 0 Carrier Fighter Model 21.  The A6M2 Model 21 was the version utilized at Pearl Harbor and throughout the Pacific, during the early stages of the war. With its maximum speed of 288 kt @ 4,550 m and ability to climb to 6,000 m in 7 minutes 27 seconds, it possessed an ascendancy over any other fighter type in the Pacific. When the war began on December 7, 1941, the Japanese Navy had 328 A6M2s in first line units. *

Rene J. Francillon, Japanese Aircraft of the Pacific War, Mitsubishi A6M Reisen (Zero Fighter). Annapolis, Maryland: Naval Institute Press, 1995. pp 362-365