Agent,
Three points of interest.
1. In TAIC (Technical Air Inteeligence Command) between the A6M5, F6F-5 and F4U-1D the F4U-1D outclimbed both the Zero and F6F-5 to 20K.
2. In test between the FW190A-5, F6F-3 and F4U-1D the F4U was superior to the F6F-3 and superior to the FW190A-5 in climbs at 140Knots (160MPH). Above that speed the FW190 was superior. Also this test was done without the paddle prop on the F4U as was installed in early 1944.
3. In climb test against the P-51B the F4U-1A (Not only the -4) the F4U outclimbed the P-51B to 20K.
Also two other notable comparisons.
Check out the climb rate chart of the P-51D/F-51D in the pilots manual. It list the climb rate at Mil power at 10,200lbs or less. Climb rate at sea level is 2400FPM and a climb time to 20,000 FT of 9 minutes. This test is dated 1953 with wing racks only and no external ordinace.
By comparison the F4U-1D flight manual list the mil power climb as 2700FPM at sea level and 8 minutes to 20K. This at 11,700LBS.
The test only show how some manufactures performance numbers can be a bit "fluffy".
In head to head test much of this is brought out into the light.
This is a great report to read. The Army test are really interesting in the back of the report. They show the P-47D out accelerating the P-51D and P-38L. Also interesting to note is how little these "Fast diving" airplanes where able to pull ahead of the Zero in a dive despite their reputations.
A6M5 vrs F4U-1D/F6F-5