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If somebody is making claims that the Ta152's wing profile provides an agility advantage, they're going to have to cough up some polars. eta: never mind; it used a NACA 230xx airfoil, with a taper in thickness. eta (again) the XP-72 used the same airfoil as the P-47, the Seversky S-3
The agility advantage resides (wing) in low drag/high CLmax, combined with high excess thrust and low wing loading. 230xx fairly common airfoil.. need more than that.
@pattern14 - when everything working on the Ta 152 and everything working on the P-51H, the P-51H was faster than the Ta 152.. and it was operational during WWII.
As far as the XP-72 goes it was a much bigger unknown that the TA-152, only two were built and they had different engines and propellers. the second one with the contra rotating props crashed after just a few flights so top performance may have been untested. There is also a discrepancy between most accounts claiming 3500hp for the engine and USAAF and P&W records that show 3000 hp for take-off and Military rating down low and 2400hp at 25,000ft. The USAAF and P&W records seem to show NO turbo but a remote auxiliary supercharger behind the cockpit driven by a long drive shaft. The 1st prototype may NOT have had this supercharger hooked up for many (all?) of it's flights.
Perhaps 3500hp was achievable with WER. P W records never seem to list WER ratings.
All in all, the XP-72 has too many unknowns to compare it's performance to much of anything one way or another.
Yah, the data are not exactly crystal cear, but we KNOW the P-47J was faster than any Ta 152 or Fw 190 derivative. It is well documented.