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No time to elaborate right now. But in my quick without much thought opinion,
I'd go with the Corsair all the way... If the battle was over water and 400 mls.
from base.
If you are talking a quick one on one mix it up dogfight, and the Spitfire has
the standard wing, the Spitfire has the immediate advantage.
As a British national I would love this to be true but it is one of many myths that will not lay down and die. From the dawn of military aviation the pilot actually sat behind the observer, this changed when a rear gunner was introduced, same in dual controlled WW1 aircraft. Landing on a curved approach was absolutely normal in the UK and USA just not absolutely normal on carriers. The problems were not just with the method of landing but also detailed problems of putting a carrier plane into service, like float and stall characteristics on the wings and rebound performance of the landing gear.My Dad served with the 4th Division, USMC, at Roi-Namur, Saipan, Tinian, and Iwo Jima, a forward observer for Naval fire support, and Marine Corps Pilots. (As usual, the Navy couldn't figure out how to land such a long nosed beast on a carrier (which you would have thought might be important in a plane designed fo carrier operations. The British figured it out, a long sweeping turn before lining up at the last instant, but it took a skilled pilot)
.
...The Seafire, the carrier based Spitfire variant, was a disaster. They took a brilliant land based fighter, made it heavier with landing gear capable of absorbing carrier landings, added a a tail hook, and just ruined a beautiful, high speed aircraft and destroyed it. Initial rate of climb reduced from 1150 meters per minute to 850. Maximum speed was reduced from 639 knots @5400 meters to 565. Empty weight increased by nearly 100 kg.
I could also point out that no comparison could take place until June 1943 for carrier operations and February 1943 for land operations, this is five years after the Spitfire was operational and two years after the first seafires.Hello David
you probably mixed knots and km/h in the speed part. Was Seafire a disaster, I don't know. At least it was short legged and at least the initial version was a bit fragile for carrier, at least CVE, use. But e.g. Corky Meyer, the chief test pilot of Grumman, loved it as a flying machine when he had an opportunity to fly Mk III at Fighter Conference in 1944, noting "I have never enjoyed a flight in a fighter as much before or since or felt so comfortable in a plane at any flight attitude." Neither have he anything untowards to say its low level rate of climb.
I'll add this topic related view lifted from a Kiwi Corsair pilot's memoir, 'Too Young to Die'.
It concerns military flying in Nippon, by occupation forces, soon after cessation of hostilies,
when 'British Empire' units 'did their bit' alongside US forces.
"Our flying duties consisted of daily patrols of the various prefectures in the British area by flights of two aircraft,
including RAF & Indian Spitfires, & Australian Mustangs from their respective bases...
...the Spitfires used by both the RAF & Indian squadrons were Mk 14, clipped wing, 2,000hp Griffon models,
fitted with 5-bladed props, & mostly with bubble canopies...
...During these patrols we would sometimes engage in in friendly dogfights with the Mustangs, but never
with the Spitfires, which were mostly forbidden to perform aerobatics at lower altitudes, due to the limited
experience of their pilots, & the frightening performance of their aircraft,
which were capable of climbing at 5,000ft per minute...
...The 5-bladed 2,000hp Griffon-engined Spitfires which frequently visited our base had however,
considerably higher performance than either Mustang or Corsair - I did one day formate on two
Spitfires approaching Iwakuni, & instead of my usual 30" boost I had to open up to 45" to stay with them.
When pilots of the Indian Spitifire Squadron performed aerobatics overhead, the incredible performance,
& deafening screech of the Griffon - was almost frightening."
We're a sad bunch!
I think you can make any WW2 fighter 20 mph faster in combat, simply by removing useful bits, like armour glass windscreen, pilot armour, rear view mirror etc. etc., perhaps even going as far as removing most if not all its guns. I think you need to look at the Kurfust data in that light. A good example is the Bf 109F-1/2. RAE tested one at 362 mph; Soviet tested one at 342 mph; Wikipedia says 382 mph. I know who I'd believe, the RAE and the Soviets as their speeds were planes that had actually been used in combat as opposed to factory fresh, polished and with any wrinkles smoothed out with putty filler.I only use official military or (second choice) factory performance
test figures when I post. The Bf.109F-4 was cleared for 1.3 ata
when it was introduced into service. It was later cleared for 1.42
ata in January 1942. From all the sources I have read to date,
they generally point to the maximum speed of 390 mph. at
6,700 m. (21,982 ft.)
I do however know of one testing on 11 July 1942 that recorded
394 mph./6,000 m. using 1.42 ata boosting.
I have not seen any evidence to date that would support the
fact that any fully operational Bf.109F-4 could reach 400 mph
(643.9 km/h) at any altitude.
I think that the German performance figures allow for a tolerance of +-5%, so if the RAE says 390 mph for a Bf 109F-4, that is the mean; 410 mph is possible, as well 370 mph. Although Kurfust does present the highest figures, he also presents the Allied figures. So a Me 262 could have a top speed ranging from 485 - 540 mph.No, I have heard elsewhere that Kurfurst cherry picks what data he posts. I think that is the issue with him. His data is not incorrect or fraudulent it is incomplete and therefor does not show the whole story.