You are saying that clipping wingtips will not affect climb rate.
If you go and check my first post on this thread you'll see what I said. I said that a small change won't make a difference, especially considering the topic; A6M2 vs. A6M3. Obviously, if you remove the wing area completely the aircraft won't do much climbing...
You are saying, explicitly, that a plane with more weight and less wing area will climb better with a mere 100 hp or so?
It all depends on how big of a change occurs for each of these parameters but normally, the more excess thrust the better the climb rate. Simply because there's more power available per the weight that is being lifted against gravity. I've already explained this earlier in this thread. But if you don't believe me, read here about
climb performance. And try to pay attention. Like I've said many times on this thread, the hp difference between Sakae 12 and 21 is 190hp, not 100hp or 150hp.
Japanese pilots thought the climb rate was worse than the model 21.
If you stating this as an argument, I'm sure you can then quote these Japanese pilots here, right? Sources, please.
Time to climb numbers seem to indicate the Zeke32 took more time to get to alt thand the model21 did.
The climb times given in Rene Francillons book say just the opposite. What is your source which claims that it took A6M3 longer to climb to any specific alt?
I gave you a nearly perfect example which you ignored:
In-game we already have the perfect example of how clipping wingtips affects climb rate. Spit8 and Spit16.
The reason I ignored it is because we are talking about Zeros here. I'm not gonna start double checking Spit figures to humor you. Lets keep the discussion in the planes this topic is about.
Once the pilots decried the poor range (made worse by the new engine sucking gas faster than the previous engine) and the lack of manuverability, the fuel was upped and the wingtips restored. This jumped up to 220kg more than the model22! It weighed almost as much as the later A6M5b but without the actual performance to go with it.
I know the range was reduced. Has nothing to do with the discussion about the climb rate though. Hmm...Model 22 (also refererred to as A6M3a) came after the A6M3 (Model 32). Model 22 actually weighed more than the A6M3 (Model 32), not the other way around.
Loaded weights from Francillon:
A6M2 (Model 21): 5313lbs
A6M3 (Model 32): 5609lbs
A6M5 (Model 52): 6025lbs
A6M3a (
Model 22) weight in Japanese literature is listed as 5906lbs, 297lbs more than the Model 32.
So, the difference in weight between the A6M2 and A6M3 (Model 32) is 134kg.
So, 100 [edit: 150?] extra horsepower overcomes 500lbs extra weight plus less lifting capacity due to clipped wings?
As you can see above, my figures tell a different story.
Compared to the A6M2, A6M3 (Model 32) gained 295lbs in weight, not 500lbs and had 190hp more power, not 100hp or 150hp.
These translate to power loadings:
A6M2: 2,57 kg/hp
A6M3: 2.25 kg/hp
You're going to have to prove that one, Wmaker, before others buy your hunch.
It's you who has "a hunch" and it's you who hasn't provided any proof.