J
apanese say ~380 mph top speed.
The source for that is a book in Japanese: Watanabe, Yoshiyuki (2000) "Shiden Kai of Local Fighter", Gakushu Kenkyusha p.180
But typical of Japanese sources, they were probably using Military rating and not WEP. There's also the question of whether this was a prototype or production version and whether it was a quote from a designer or from a pilot.
Compared to Japanese performance test conditions, very high-octane fuel would certainly not hurt, but would be unlikely to significantly improve speed performance. That is, unless modifications were done to run the engine at higher performance than design, which is unlikely.
Greg dug up the original source documentation and said it was 96-octane, not 100 or 92.
I myself am highly dubious that a Japanese 2,000 horsepower engine somehow produces a slower aircraft than a US 2,000 horsepower engine, all things being equal (let alone when factors like weight and drag are leaning heavily into the Japanese aircraft's favor, as is the case say, if you compare an N1K to an early to mid- run P-47.)
The N1K1/2 suffered from aerodynamic drag factors that was a legacy of its floatplane origins. While it had an excellent wing design featuring a low-drag airfoil, that was offset by the 4-degree attachment point between the wing and the fuselage (if I understand correctly, I could be wrong). Basically, Kawanishi rushed a design into production because they knew the Navy had no good alternative.
The Shiden Kai retained the crappy attachment point, which caused a degree of performance loss. Overall, the success of the Shiden was the result of a combination of shrewd political maneuvering between Kawanishi and Genda (who was Kawanishi's inside man in the IJN) and corruption. It definitely was a technically sophisticated aircraft but it took over a year of development to eliminate its horrendous failings. An aircraft that writes itself off in landing accidents more often than it gets shot down is a horrible aircraft.
The Japanese planes may be faster than some credit them with. But are they 420mph airplanes?
This is an interesting subject. Francillon himself said that the
late-war, partially wooden Frank II made 416 MPH with the -23 and -25 models of the Homare, but didn't include a source. However, everyone points at Francillon's
equally unsourced numbers when they say that the Frank wasn't as fast as TAIC's calculation. I personally believe that the early Pe-32 prop's pitch angles and length wouldn't have allowed the full horsepower to be deployed but for everyone who is treating Francillon's numbers as fact, his numbers for the Frank II are just as valid: 669 kph. That's not much different from the 687 KPH calculated by TAIC.
Again, let's be clear about this: Francillon was using Japanese numbers (which were without thrust stacks, without a fully rated -21 engine, without WEP, and were for prototypes).
We know that the -23 and -25 engines were direct injection and therefore had better fuel-air mix control at altitude. The -23 was likely 1900 HP and the -25 was the first fully rated 2,000HP engine.