CORSNING
Tech Sergeant
Thank you Shortround,
I studied all that info already. I was just on a roll and threw the 45M in on a whim.
I studied all that info already. I was just on a roll and threw the 45M in on a whim.
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The Spitfire II and V had the performance to dominate the Japanese Ki 43 and to a lesser degree the Zero,
The Mk.V possibly, the Mk.II?...My money is on the Ki.43. It easily outturned either Spitfires
and probably outrolled at least the Mk.II. Acceleration at low speeds wasn't even a contest.
Bed time for me now, but a side by side comparison of the Mk.V and TAIC Oscar using WEP
might prove very interesting.
Hi Tomo,
Ram effect is not present unless there is a straight or almost straight shot to the carb. If you have roundabout way to the carb, a FOD separator, and a plenum with exit, ram is not present. The Hellcat was rather well known for NOT having ram effect in the main stage. As a result, it never suffered a carb icing crash in service. The Corsair cannot say the same. The Hellcat DID have higher operational losses when not in combat. Maybe it was a case of being there while the Corsair was not? The Corsair was late to the party. But they both used the same engine and prop until the F4U-4, so reliability would likely be very similar.
If you fly the Hellcat and the Corsair, both in main stage (no S/C) and both with 3-blade props, there is little to no difference in speed at similar power settings. With ram, yes, the Corsair had a better ram setup. The achievements of both types are well known and the Hellcat did better by a long shot. Opportunity due to being there? Maybe.
I am inclined to believe the Corsair was a better fighter, but you certainly can't prove it with actual war record achievements, can you? Good thing they were both on the same side. It would be tough to choose between them for me. Most in here would likely choose the Corsair, probably including you, but I'd likely opt the other way.
Hi Tomo,
The Corsair was late to the party. But they both used the same engine and prop until the F4U-4, so reliability would likely be very similar.
Greg,
I do not want to take away anything from your Post #186. My purpose here is just
to make a slight correction in one of your statements.
The F4U-1 and F4U-1A used the 13' 4" blade design No.6443A-21 or 6525A-21.
Hamilton hydromatic type 23 E50 hub.
The F6F-3/-5 used a 13' 1" blade design No.6501A-0 AFAIK.
The first Corsair to use the 13' 1" propeller was the USN F4U-1D.
Mike & Neil, If you guys are still watching I thank you both for the excellent
information you have provided to all.
Nothing in warbird community is being driven above MP, all are much lighter with no guns, no full combat load out of fuel, etc. so there is nothing to talk about as far as modern day comparisons to fighters being hammered at 80" boost and 150 octane fuel compared to 57-61" and 100LL
You guys never cease to amaze me.