Originally posted by funked:
Widewing, the same technique you used to show that the N1K2-J did not have more than 1400 hp will show you that 3450 hp will not make a P-47 go anywhere near 480 mph at sea level. I have a feeling somebody misprinted the altitude or speed, or forgot to mention that the plane dove from 10,000 feet. 
I calculate a HP/f ratio of 540. That's better than twice that of the F6F-5. The P-63A, which can attain about 390 mph at sea level has a HP/f ratio of 293.
Required thrust to attain and maintain 480 mph is:
375 x .80 x 3,450/480= 2156 lbs
With regards to the Republic test data: All test hops mentioned utilized instrument panel cameras to record all readings. In addition, the airspeed measuring system was calibrated prior to each flight. I recall that each speed run was begun at 200 ft (over Long Island Sound)and 200 mph. From this baseline, the pilot went to full power and maintained this until the aircraft stopped accelerating. For comparison, did not the Tempest prototype top 470 at sea level?
My regards,
Widewing