Simon Thomas
Senior Airman
Those who were there called it the "Kokoda Track".
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A possibility, which I have not checked out, is that the P-39 had a higher wing loading and perhaps not as good RAM. P-39s seem to have peak power a bit lower than P-40s in fight tests. Look for where the intake pressure drops off in both level speed and climbing. The cockpit canopy may had disturbed airflow and/or the intake scoop was not as good as the P-40 duct?For reasons I don't understand, the P-39s of all types seemed to have more trouble both climbing to altitude and flying at altitude than the P-40s did, in spite of their having nearly identical mid-altitude rated engines and P-39 having a better initial climb rate, at least on paper.
The location of the P-39's intake was terrible. It seems to me that the intake on the side or underneath the fuselage would have been a much better decision.The cockpit canopy may had disturbed airflow and/or the intake scoop was not as good as the P-40 duct?
The location of the P-39's intake was terrible. It seems to me that the intake on the side or underneath the fuselage would have been a much better decision.
I think we have discussed the phenomenon of smaller wings maybe not being as ideal in the Tropics and maybe performing a bit better in the cooler climate and / or downright cold air.
That might be a possible explanation for some of the P-39s troubles in the South Pacific, and maybe the Buffalo as well as it also had relatively small wings.
I thought the Buffalo was a nimble little fighter with rather low wing loading—the engine performance was disastrous, not the airframe. Please correct me if I'm mistaken.
The export Buffalo for Finland had the R-1820-G5, rated at 950 hp. The USN's F2A3 had the R-1820-40, rated at 1,100 hp.I thought the Buffalo was a nimble little fighter with rather low wing loading—the engine performance was disastrous, not the airframe. Please correct me if I'm mistaken.
Hey Greg, you're well versed with the B-26 - would you happen to know how the heat in the SWP affected the B-26's take-off versus ops in the ETO?Finnish B-239s were initially armed with one .30 and one .50 in the nose, a .50 in each wing. They later e changed the .30 for another .50.
RAF Buffalo Mk Is and US F2A-3s were armed with four .50s.
Though efforts to lighten the aircraft and improve realiability resulted in a variety of gun mixes.
Some good stuff about Brewster F2As here.
Brewster Buffalo: differences from F2A to 339E https://share.google/ByMNdLWQnQQp3FhLW
These things were all over the place on weight. In part because of some rather dubious weight charts. Like how many 239s flew with just one .30 cal and one .50 and just 100US gal of fuel?they were roughly 350 - 400kg lighter, with an engine with 100 - 150 less hp.
All I had available at the moment, were specs for the -IIb, however, this also drives home the wing-area comparison.View attachment 896409
The original Ki-43-I (the only type available through mid 1942 in China and Burma, mid 1943 in the South Pacific) had a 37.6' / 11.44m wingspan and a wing area of 22 sq m / 236.8 sq ft.
View attachment 896410
The Ki-43-II had the shorter (and also stronger) wings and a lot of other improvements.
The export Buffalo for Finland had the R-1820-G5, rated at 950 hp. The USN's F2A3 had the R-1820-40, rated at 1,100 hp.
In regards to the wings, the F2A3 had a wingspan of 35ft. with an area of 209 sq/ft.
The P-39D had a wingspan of 34 ft. with an area of 213 sq/ft.
The A6M2 had a wingspan of 39 feet, 4 inches with an area of 241.5 sq/ft.
The KI-43-II had a wingspan of 35 feet, 7 inches with an area of 230 sq/ft.
The hot air in the SWP put the F2A (and it's Commonwealth types) at a disadvantage as well as the P-39. The hotter the air, the lower the density, which decreases lift. This is one reason why the 239, even with it's lower hp rating, performed so well in Finland. The same can be said for the P-39 on the Eastern Front.
Wouldn't wing loading matter more than absolute wing area with respect to lift? I'm a little confused still.
Surely the Zeke and the Oscar had some of the lowest wing loadings of any front line fighters during the war, so I get the relative advantage there vs allied types of any sort.
A P-39D may have had a slightly larger wing, but it also weighed like 20 percent more than an F2A. I figure the wing loading on the Buffalo was considerably lower—lower than a P-40E even. And the P-40 was a perfectly effective fighter in the South Pacific—it certainly had a much better reputation than the Airacobra among allied pilots in New Guinea, didn't it?
The wing loading question in hot climates is certainly interesting and one I hadn't given much thought to!