In!
Answers from another forum: "BuAer evaluated an FW-190 after the war against the F6F and F4U. The report observed that the FW-190 climbed faster than either of the Navy's best fighters, but that both the F6F and F4U had tighter turning radii at higher speeds. The tactical discussion suggested that if a F6F or F4U was attacked by an FW-190, the Navy should use its superior turning performance to gain advantage on the FW-190. Most tests showed the F4U and F6F gaining advantage in less than one full turn. On the offense, BuAer suggested that it would be difficult to close on the FW-190, so a high angle off attack should be used. Finally, the report observed that the FW-190 had the disconcerting habit of not signally a stall, but stalling abruptly followed by aileron reversal. That made the aircraft very difficult to control at low speeds or high angles of attack.
The BuAer test pilots especially liked the visibility afforded by the FW-190, but otherwise observed that its' engine controls denied them the type of control over the full range of the engine's abilities that the more conventional Navy Throttle, Mixture and Propeller levers. The FW-190 used several electro-mechanical devices to "automate" engine control that took away pilot discretion. Conversely, the Navy used simple lever controls for the three major engine inputs. The aviators were free to manipulate throttle prop and mixture as needed and through their full range of power settings.
My take from the report, all things equal the FW-190 could dictate the time and place of any engagement with the F4U or F6F. The F4U or F6F could generally dictate the outcome of the engagement because once in a fight, the FW-190 could not stay with the F4U or F6F. The only viable offensive move for the FW-190 was a "slash and dash" attack utilizing the type's superior speed in climb and level flight."
There's more opinions at the link.