There was a discussion on merits of a V-12 powered Fw 190, in early years. Perhaps this graph could mean something, both to proponents and opponents

The original (black lines) is from the manual for the DB 601E-G engines, the colored lines are for the BMW 801C for Notleistung (red) and Kampfleistung (pink), from this
table. There are some caveats to it, however.
Caveats - the Notleistung was not available for the DB 601E during 1941; from December 1941/January 1942 the BMW 801C should be able to use 2700 rpm also in second S/C gear (per tests linked before; that would mean at least 1400 ps at 5 km? no ram). Then we have the question of ram air intake - we might call it 'very good' for the DB 601E, and 'not that good' for the vast majority of the historical BMW 801 installations (and for all BMW 801
C installations); the importance is that better layout of ram air intake will benefit the engine 'breathing', hence more power is gained at altitude.
Next - the engine-related drag. The Fw 190A8's equivalent flat plate for fuselage was 0.156 sq m, and for the cooling it was 0.073, for the ram air intakes it was 0.003 = total of 0.232 sq m. For the Jumo 213A, we have 0.1393 sq m for fuselage, 0.039 for cooling, and 0.019 for ram air intake = total of 0.1973 sq m. Granted, not all liquid-cooled engines' installations are created equal, but we can be sure that a V-12 will make a tad less of drag than, even a well executed, radial engine installation. (the equivalent flat plate, for high speed, was 0.485 sq m for the 190A-8 A-9, and 0.444 for the 190D-9)
At the end of the day - looks that whatever the BMW 801C offers in raw power, the DB 601E can compensate in the drag, weight and consumption reduction, except for low level capabilities.