Can we make a faster better performing Wildcat in 1942?

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Wild_Bill_Kelso

Senior Master Sergeant
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Mar 18, 2022
The Wildcat was a 'pretty good' naval fighter. Grumman had to walk the fine line between everything you need to operate from a carrier, including the fuel needed to fly long missions and stay up for CAP for hours at a time, vs the performance needed to contend with enemy fighters and shoot down enemy strike aircraft - as well as enough guns to do both jobs. All with a moderately powerful engine at best. It was a very difficult task.

The F4F-3 was a decent compromise. Just at the line of acceptability if slightly below it. It wasn't fast but a two-stage supercharger meant that it still had some pep at altitude, which was a saving grace.

But when they decided they needed folding wings, they made the F4F-4, which climbed like an overloaded truck, and had inferior speed. It allowed for 50% more aircraft on the carrier, which definitely helped, but the power of the (1200 hp, R-1830) engine was not increased while the weight certainly did increase, and the result was fairly dismal. The same can be said for many of the earlier Martlet types used by the British.

Eventually, though far too late IMO, they came out with the FM-2, with 1350 hp Wright 1820-56. My understanding is that this was made possibly due to technical improvements in cooling fins made during the development of the lager Pratt and Whitney R-2800. That extra 150 hp seemed to really improve performance, such a climb rate, but at the expense of losing the two stage supercharger.

The problem is that between the F4F-4 and the FM-2, there was about a year and a half where the USN (and to some extent the USMC and the RN) had to rely heavily on the F4F which was overloaded and underpowered. Meanwhile Japanese and German aircraft were improving. The Japanese got the improved A6M3 and Ki-43-II, as well as the Ki-61 and Ki-44. They also got the fast B6N torpedo bomber. The Germans got the scary Fw 190 and improved models of the Ju 88. F4F-4 is falling way behind these types in 1943.


I can see in the history of the Pratt and Whitney R-1830 double wasp that they did eventually make some variants with 1350 hp, starting with the R-1830-75, and then the R-1830-94. I assume these were either not ready, or too late. I know the focus for Grumann and the Navy was on the Hellcat, with good reason, and Chance- Vought was developing the very promising Corsair. But I think they needed a stop-gap. Could they have made a clipped wing, 4 gun, lighter Wildcat? Could they have gotten the R-1830-75 or 1830-94 working reliably a bit earlier with some more effort?

What I'd really like to do is make one which is a bit longer and less stout. But I realize that is probably impossible so I'll settle for clipped wings and 150 more horespower. It seems like that should be in reach.


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Looking at the Wildcat, it seems like the designer just didn't want to taper the fuselage at all. I realize they had to accommodate the diameter of the engine, bud did it really need to be that wide all the way back?
 
Ok, a number of things.
Eventually, though far too late IMO, they came out with the FM-2, with 1350 hp Wright 1820-56. My understanding is that this was made possibly due to technical improvements in cooling fins made during the development of the lager Pratt and Whitney R-2800.
I don't think that P & W was sharing much of anything with Wright. I don't have the exact history of the Wright cooling fins but they wound up being used on the "Later" R-3350s, Later means after the B-19 not the B-29. They were also the part of difference between the 1700hp R-2600s and 1900hp R-2600s.
Wright had done another one of their "redos" of the R-1820 where they kept the bore and stroke and changed just about everything else. Yes they used the new cylinder fins but they also changed the cylinder heads, the crankshaft, the crankcase, and a bunch of the smaller parts. They also used 20 bolts to hold each cylinder to the crankcase instead of the 16 they used on most the cylinders since the early to mid 30s (?). BTW they had to change the crankshaft to get 1350hp out of the -56A, the -56 was good for 1300hp.
can see in the history of the Pratt and Whitney R-1830 double wasp that they did eventually make some variants with 1350 hp
Yes they did. In this case it was using stuff they developed from the R-2800. It was sort of trickle down. Once they developed it for the R-2800 they looked at applying it to the R-1830.
Could they have gotten the R-1830-75 or 1830-94 working reliably a bit earlier with some more effort?
That may depend if you want to slow down the R-2800 any?
A 1350hp R-1830 was not going to be a war winner, the R-2800 was.
The next thing is that you don't really gain much. It appears that they didn't change the supercharger much. The power at altitude is not that much different when you consider they increased the Engine RPM From 2700 to 2800 (they change the bearings). On the two speed engine in high gear they went from 1050hp/13,100ft to 1100hp/13,750 ft. Engine also gained about 80lbs.
Things were better on the turbo engines but that is a much harder change for the Wildcat.
I realize they had to accommodate the diameter of the engine, bud did it really need to be that wide all the way back?
It may not have had to be as wide but it did have to that tall if you are going to keep the view over nose.
All of the fuel and oil was inside the fuselage under the wing. Maybe it didn't have to as wide as it was but you are hiding 144US gallons fuel and 11 gal of oil in the belly.

You really don't gain much by clipping wings, and you often loose a lot.
Increased landing speed.
Longer take-off distance.
Decreased range.
Greater turning circle.
Lower Ceiling.

Strangely you can often get a bit better climb rate but that depends on the Altitude/air density. Better at low altitudes vs worse at high altitudes.
 
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No replacement for displacement: R-2000 is more/less R-1830 with 5.75" cylinders instead of 5.5". 150 extra ponies at cost of 300lbs weight

We must remember, the XF4F-0 was a biplane - Grumman went too conservative with the upgrade of the F3F.
 
No replacement for displacement: R-2000 is more/less R-1830 with 5.75" cylinders instead of 5.5". 150 extra ponies at cost of 300lbs weight

We must remember, the XF4F-0 was a biplane - Grumman went too conservative with the upgrade of the F3F.
Also they "seem" to have kept the supercharger from the R-1830 engine.
The higher power levels were only available at lower altitudes than the R-1830.
They may have got a bit more power but nowhere near the changes in take-off power show.
 
Off-the-shelf engines, or something plausible that was not available?

Either. I'd like to know the history of the R-1830-75, numerically it falls before the R-1830-76 used on the F4F-3. Maybe it used too much fuel? Looks like it had more potential.
 
Ok, a number of things.

I don't think that P & W was sharing much of anything with Wright. I don't have the exact history of the Wright cooling fins but they wound up being used on the "Later" R-3350s, Later means after the B-19 not the B-29. They were also the part of difference between the 1700hp R-2600s and 1900hp R-2600s.

It sounds like I confused P&W with Wright

Wright had done another one of their "redos" of the R-1820 where they kept the bore and stroke and changed just about everything else. Yes they used the new cylinder fins but they also changed the cylinder heads, the crankshaft, the crankcase, and a bunch of the smaller parts. They also used 20 bolts to hold each cylinder to the crankcase instead of the 16 they used on most the cylinders since the early to mid 30s (?). BTW they had to change the crankshaft to get 1350hp out of the -56A, the -56 was good for 1300hp.

Yes they did. In this case it was using stuff they developed from the R-2800. It was sort of trickle down. Once they developed it for the R-2800 they looked at applying it to the R-1830.

I think this is what I misconstrued for the higher HP R-1820. But couldn't they have done this sooner? When did the R-1830-75 come out, do you know?

That may depend if you want to slow down the R-2800 any?

Definitely do not want to slow down the R-2800

A 1350hp R-1830 was not going to be a war winner, the R-2800 was.

Agreed, but I still think there is some space between the 1,200 hp engine and the 2,000 hp

The next thing is that you don't really gain much. It appears that they didn't change the supercharger much. The power at altitude is not that much different when you consider they increased the Engine RPM From 2700 to 2800 (they change the bearings). On the two speed engine in high gear they went from 1050hp/13,100ft to 1100hp/13,750 ft. Engine also gained about 80lbs.

I'm definitely not worried about the 80 lbs for 150 hp. And I think if that extra HP is mostly at lower altitudes, I still like that. It will help with takeoff, it will help with escape maneuvers (diving down to the deck and pouring on the coal to escape), it will help against torpedo bombers, and it will help with initial climb rate at least for the first couple of minutes. Get you up to 6-8,000' a little faster, that will cut the overall time to altitude by a good bit. And by the time your engine is flagging a bit, the air is getting thinner too.

Things were better on the turbo engines but that is a much harder change for the Wildcat.

Definitely don't want to put in a new turbo. But how feasible is it to make an improved supercharger?

It may not have had to be as wide but it did have to that tall if you are going to keep the view over nose.
All of the fuel and oil was inside the fuselage under the wing. Maybe it didn't have to as wide as it was but you are hiding 144US gallons fuel and 11 gal of oil in the belly.

1930s fighter designers seemed to have a penchant for making short, fat, squat planes. I-16, I-15/ 153, F2A, F4F... It seems like you ought to be able to fit the same amount of fuel and oil in a bit slimmer fuselage if you stretched the fuselage (i.e. lengthened) a little bit. You could then conceivably squeeze it and make it a bit more streamlined (once past the engine) like they did with the Hawk 75

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You really don't gain much by clipping wings, and you often loose a lot.

That depends how much you clip the wings. For the Wildcat even 1' would help a bit I think, without having a major effect on range or turning circle. The A6M5 had 3" shorter wings than the A6M2 but it did not lose much in maneuverability. Slightly shorter wings also increases roll.

Increased landing speed.
Longer take-off distance.
Decreased range.
Greater turning circle.
Lower Ceiling.

Strangely you can often get a bit better climb rate but that depends on the Altitude/air density. Better at low altitudes vs worse at high altitudes.

That would be due to reduced drag, which is what we are going for here.
 
Army numbers and Navy numbers are not in sequential order in relation to each other.
Army numbers are in ordered and Navy numbers are in order but there could be 1 - 2 years difference between the Army and Navy numbers.

Ah gotcha.
 
The 6 guns get a lot of the Blame.
I am not saying that the 6 guns were a real good idea, just that they get all of the blame for the wing fold, the 150lbs of self sealing material for the fuel and oil tanks and the 120lbs of pilot protection.

Difference between 4 guns with 430rpg and 6 guns with 240rpg was 63lbs. The 4 gun planes didn't have to carry 430rpg and with 330rpg they could save about 120lbs.

The early Martlet Is may have had the slow firing early .50 cal guns, which jammed a lot, and they used the older lower velocity/lower powered ammo.

I don't KNOW if that had any influence on the British decision to ask for 6 guns but it does seem plausible.
 
When did the R-1830-75 come out, do you know?
It was used in a few DC-3s (which tells us nothing) and it was used in a few (8?) pre production B-24Ns with turbos. The rest of the B-24Ns were canceled Here is the extreme of the the number system The USN -72 engine was used the PBY-4, they used a later engine in the PBY-5.
The Navy -94 engines were used in PB4Y-2s

Agreed, but I still think there is some space between the 1,200 hp engine and the 2,000 hp
Maybe but it is a bit iffy, nobody put a R-2000 into combat plane.
P&W had given up the first version of an R-2180 (14 cylinders using R-2800 cylinder dimensions but not real R-2800 cylinders)

I'm definitely not worried about the 80 lbs for 150 hp. And I think if that extra HP is mostly at lower altitudes, I still like that. It will help with takeoff, it will help with escape maneuvers (diving down to the deck and pouring on the coal to escape), it will help against torpedo bombers, and it will help with initial climb rate at least for the first couple of minutes. Get you up to 6-8,000' a little faster,

See above about the R-2000, the boost in power was at really low altitude. The -94 was good for 1350hp at 2,000ft. the Standard two speed R-1830 was good for 1200hp at 4900ft.
the -94 may have been down to around 1270-1280 hp at that altitude (both are without ram).

Another problem here is that you can't overboost the radials like you can Allisons or Merlins, they will either blow up or melt down much more often. A few crews did it and lived but they were using multi engined aircraft and the engines were junked when they landed.

To get the extra power you need the new cylinders with new cooling muffs and you need the new bearing (and crankshaft/crankcases?) you don't drop plain bearings into a crankcase/shaft set up for roller bearings.
 
Also they "seem" to have kept the supercharger from the R-1830 engine.
The higher power levels were only available at lower altitudes than the R-1830.
They may have got a bit more power but nowhere near the changes in take-off power show.
They didn't put much effort into R-2000 (only handful of variants), and I haven't seen a 2 stage (and P&W 2 stage is really 3 speed - neutral, low and high on 2nd stage). With >5k produced, it couldn't have been that bad. 1,450hp for the R-2000-7M2 (DHC-4A) is a quite a bit more power.

British were also trying to shoot down Luftwaffe MPA with self sealing tanks, armour and decent for period defensive armament (4- 7.92mm, 1 - 13mm & 1 -20mm). RAF had also learned that there was serious skill difference between an average pilot and an ace. The average pilot needed the extra firepower.
 
XF4F-1 contract 46973 dated 2 March 1936, biplane, not built, evolved into contract 63072 dated 3 October 1938 for the XF4F-2 then XF4F-3, BuNo 0383 Engine P&W XR-1830-76

"Replaces XF4F-1 design. Returned to contractors works for modification from XF4F-2 to XF4F-3 in August 1938. Delivered Anacostia in April 1939 for trials as XF4F-3 C-63072. Returned to contractors works June 1939. Finally accepted August 1939."

In 1939/40 USN Aircraft on order with R-1830

-64 TBD-1
-68 XPBS-1
-72 XPB2Y-1, PBY-4
-78 PB2Y-2
-82/92 PBY-5
-90 XF4F-6

Engine Ratings are BHP/RPM/Feet, USN Aircraft performance
ModelF4F-4F4F-3
EngineR-1830-86R-1830-86
Take-Off1,200 / 2,9001,200 / 2,900
Normal1,100 / 2,550 / 0-3,3001,100 / 2,550 / 0-2,500
Normal1,080 / 2,550 / 3,800
Normal1,090 / 2,550 / 11,3001,050 / 2,550 / 12,000
Normal1,030 / 2,550 / 13,000
Normal1,040 / 2,550 / 18,4001,000 / 2,550 / 19,000
Military1,200 / 2,700 / 0-1,8001,200 / 2,700 / 0-1,800
Military1,135 / 2,700 / 3,400
Military1,150 / 2,700 / 11,5001,150 / 2,700 / 11,500
Military1,030 / 2,550-2.700 / 15,000
Military1,040 / 2,550 / 18,4001,000 / 2,550 / 19,000

http://www.enginehistory.org/Piston/P&W/R-1830/R-1830Index.pdf

The Twin Wasp SC10 R-1830-75 was built by Buick which made its first R-1830 in February 1942. Trouble is Buick production is listed under C4G apart from a run of C9G in 1945, so no information on when -75 production began but B-24N production was 7 in 1945.

F4F-4/FM-1 production from November 1941 to December 1943.
F4U-1 production from July 1942.
F6F-3 production from September 1942.
FM-2 production from September 1943.
 

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NACA was experimenting with individual exhaust stacks on the XP-41 and XP-42 by the winter of 1941/42. Apply these on the F4F and there is a 10 mph gain? It was one of the things that were applied eventually on the FM2, as well as on the F6F before it.
Two oil coolers - have these installed in the wing leading edges instead of them being underslung in SPitfire fashion - shave some drag - gain another 5 mph?
(FM2 had oil coolers relocated in the engine section due to the R-1820 needing less space than the 2-stage R-1820)
Keep just 4 HMGs - again 5 mph and some speed and RoC gain?

Best case scenario of 20 mph gain, realistic scenario of 15 mph gain?

A more adventurous F4F would've have the 2-stage R-2180 installed (remained a paper project only), or at least a 2-speed supercharged version. However, that engine was discontinued by the P&W before ww2, and the small sibling of the R-2800, the R-2180E, is too late for this
Even more adventurous F4F would've have the R-2600 in the nose. Another candidate, had it ever materialized, would've been the 'short stroke cyclone' R-2170; 1700 lbs as a 1-stage engine, and 1800 as a 2-stage. 1500 HP was expected on 2900 rpm.
 
individual exhaust stacks
Doesn't cost much but better for speed than climb.
Two oil coolers
I am not sure how much is drag from the housing (fixable) and how much is drag from the internal air flow
Keep just 4 HMGs - again 5 mph
A lot of drag from two gun muzzles and two ejection ports?
Even more adventurous F4F would've have the R-2600 in the nose
F4FtorchNoseOverLand.jpg

Yep, lets stick another 4-500lbs in the nose!
Grumman had already looked at this twice, and twice they figured they would be better off with a new airframe.
 
Keep just 4 HMGs - again 5 mph and some speed and RoC gain?

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What were the 20mm guns on the Spitfire worth?
And the speed is proportional to the speed loss, That is to say that a 5mph speed loss at 375mph means only a 3-4mph loss at 330mph.
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These were only supposed to be good for an 8-10mph speed reduction from the eight .303s.
Maybe they cost a bit more but you can barely see the extra gun in the F4F-4s wing.
 

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