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Until folding-wings were adopted, the Buffalo was the only British monoplane, single-seat fighter that could fit onto HMS Hermes' lifts. So, if we want Hermes to have a single-seat monoplane fighter, the Buffalo is your only pick. Beyond that, best to leave them in Malaya. I calculate 14-16 should fit in Hermes hangar. I omitted the forward lift below, but the space is correct.which is the better fighter plane? The Finns felt the Brewster was nuch better then the Russian Huricanes and several piolets that flew both preferred the Buffalo. What if they had used the naval version of the buffalo instead of the Sea Hurricane?
which is the better fighter plane? The Finns felt the Brewster was nuch better then the Russian Huricanes and several piolets that flew both preferred the Buffalo. What if they had used the naval version of the buffalo instead of the Sea Hurricane?
The Winter War was before the introduction of the MiG, Lavochkin and Yak fighters. The Buffalo can compete fine with the I-16 and I-15. Give the Finns eight gun Hawker Hurricanes vs. I-16 or the Soviets MiG-3, La-5 or Yak-1 vs. Buffalo and either side clear the skies.Why the Buffalo did better for Finland...Brewster F2A Buffalo
The Finnish Buffalo pilots considered the Hurricane at low level to be an easy kill. Seems like they said "aim just in front of the cockpit and it will catch fire easily" or something like that. But the Finns had the earlier lighter Buffalo and it must have been tremendously maneuverable.The Winter War was before the introduction of the MiG, Lavochkin and Yak fighters. The Buffalo can compete fine with the I-16 and I-15. Give the Finns eight gun Hawker Hurricanes vs. I-16 or the Soviets MiG-3, La-5 or Yak-1 vs. Buffalo and either side clear the skies.
Here's a link from to a discussion on Finnish claims and losses (2009)...Finnish Air Force claims and losses (fighter squadrons) - Axis History Forum In it are five links to Finnish fighter groups (24th, 26th, 28th, 32th and 34th) claims and losses, albeit from Wiki. To save you the time the header reads.....
The list distinguishes the air victories gained by the Finnish Air Force during the Winter and Continuation War 24 and military losses.
For Finnish machines, FR stands for Fokker D.XXI, BW stands for Brewster 239 and MT stands for Messerschmitt Bf 109.
In the list, some of the Air Force are most likely recorded as the wrong type of enemy aircraft, because in combat conditions, identification was not always easy. For example, the Mustang and Spitfire aircraft were not used on the Finnish front. Mustangs are probably Jak-9 machines
Off the get-go, the 24th, with Buffaloes shot down a lot of "modern" Russian aircraft during the Continuation War
I rate the Buffalo as the worst fighter produced by the U.S.A. to be used in the war with the sole exception of the Boeing P-26 Peashooter that was pretty good when it entered service but was obsolete when WWII broke out. The success of the Buffalo in Finland can be attributed to a few points including:
1) Very poor Soviet opposition with green pilots in obsolete types, fighting over enemy territory. Anyone who went down and lived was probably lost or captured.
2) Experienced and talented Finnish pilots, fighting FOR their country over their own territory. Anyone who went down and lived was repatriated and could return to duty.
Also, the Buffalo as it served in US service didn't climb at over 3,000 feet per minute. It was more like 2,400 fpm. From all reports, it was a pleasant aircraft to fly, but not really in the fighter league. Aerobatics were "gentlemanly," not spirited. The armament was not very good, but was sufficient against lightly-built or obsolete opponents that had ever worse fighter performance than the Buffalo.
It did NOT have a 26 : 1 kill ratio as a type, only in Finnish service. When you state a kill ratio, it must include the population of the type. Otherwise, where do you stop? With one mission? I can point out missions where almost all WWII fighter types had a combat kill without loss. That doesn't mean the type had an outstanding kill ratio.
Imagine if the Finns had GOOD fighters in service!
The "Naval Version"?which is the better fighter plane? The Finns felt the Brewster was nuch better then the Russian Huricanes and several piolets that flew both preferred the Buffalo. What if they had used the naval version of the buffalo instead of the Sea Hurricane?
The "Naval Version"?
The plane was accepted by the USN for Naval use. There never was another version of the F2A-1.
Fubar's right, though. The Buff's big Achilles Heel was always it's weak (for carrier use) landing gear. One of the reasons it was replaced by the F4F and limited to land based operations only (that, and later versions of the airplane turned it into an inferior fighter. In the end, the F4F became a better plane than the F2A. Some say it always was...we all have our favourites, I guess).
Elvis
The royal navy refused to consider the Buffalo because it had no tail hook. The RAF had ordered a de-navalized version and the navy seems to have not bothered to look at the US version. The landing gear was fixed eary on in the F2A1 and did not cause issues with the F2A2. The extra weight of the F3A3 caused a different mode of failure on repeated hard landings. Thhis slow bending of the strut mount was partly due to maintenance practices. The F2A3 maneuverability was essentially equivalent to the F4F3 except for roll rate, which was better. The F2A3 was a dog compared to the F2A2 not the F4F3.The "Naval Version"?
The plane was accepted by the USN for Naval use. There never was another version of the F2A-1.
Fubar's right, though. The Buff's big Achilles Heel was always it's weak (for carrier use) landing gear. One of the reasons it was replaced by the F4F and limited to land based operations only (that, and later versions of the airplane turned it into an inferior fighter. In the end, the F4F became a better plane than the F2A. Some say it always was...we all have our favourites, I guess).
Elvis
If the problem returned, that means it was never fixed in the first place.Actually the undercarriage story is a bit more complex. Issues were found with the F2A-1 which were largely corrected in the F2A-2. Unfortunately, Brewster/the US Navy decided to build the much heavier F2A-3 and undercarriage problems started to return.
If the problem returned, that means it was never fixed in the first place.
As you can see here the whole arrangement is a compromise.
The load is supposed to be directed into the large main struts, but they're anchored out towards the end of the wing.
Should be the other way around. The root is always your strongest area.
Then there's the angle. The whole thing is a big "W". If there were less angle to the main struts, they would absorb more of the load and it would be better, but the design is still weak. It's always going to put some of the load onto the smaller articulated parts and that shouldn't be.
Elvis