WW: Is that because you think ours is the P-40C without a DT rack? I seem to recall that from a long ago discussion. Was the P-40C that much slower?
How is the P-40B doing what the P-40E is listed as doing for top speed. Less draggy nose, maybe?
EDIT: Interesting, you are on to something. It seems even the first P-40 models (before the A designation was retrofitted) made that much.
http://www.warbirdforum.com/p040.htm"The first flight of a P-40 (Ser No 39-156) was on April 4, 1940. Maximum speed was 357 mph at 15,000 feet, service ceiling was 32,750 feet, and initial climb rate was 3080 feet per minute. An altitude of 15,000 feet could reached in 5.2 minutes. The length of the P-40 was 31 feet 8 3/4 inches, which became standard for all early models. Weights were 5376 pounds empty, 6787 pounds gross, and 7215 pounds maximum."
Joe Baugher's commentary. He's not always right on every detail but I think he's pretty good compared to many resources.
Here are his comments on the -B model:
"The P-40B (Model H81B) differed from the P-40 in having an extra 0.30-inch machine gun in each wing. The engine was still the V-1710-33. In September 1940, 131 P-40Bs were procured by the Army to replace the deferred P-40s. Serials were 41-5205/5304 and 41-13297/13327. The first P-40B flew on March 13, 1941. The P-40B retained the same dimensions of the P-40, but weight was increased to 5590 pounds empty, 7326 pounds gross, and 7600 pounds maximum loaded. Because of the additional weight, the P-40B had an inferior performance to the P-40, maximum speed being 352 mph, service ceiling being 32,400 feet, and initial climb rate being 2860 feet per minute. Normal range was 730 miles, but a maximum range of 1230 miles could be attained at the minimum cruise settings."
Very interesting that throughout all the changes from slick nose to big radiator, the speed rarely changed much!
[EDIT2:]Seems even slow for a P-40C:
"The initial P-40 order was finally completed with 193 P-40Cs (company designation H81-B). Serials were 41-13328/13520. The first flight of a P-40C was made on April 10, 1941. The P-40C retained the 1150 hp Allison V-1710-33 engine, but was fitted with a new fuel system with 134 gallons in new tanks with improved self sealing. In addition, provisions were made for a 52-gallon drop tank below the fuselage. The P-40C had a SCR-247N radio instead of the SCR-283. These additions produced yet another upward crawl in the weight --- the weights for the P-40C were 5812 pounds empty, 7459 pounds gross, and 8058 pounds maximum loaded. Consequently, the performance continued to degrade. Maximum speed was 345 mph at 15,000 feet. Normal and maximum ranges were 730 and 945 miles respectively. Service ceiling was 29,500 feet, and initial climb rate was 2650 feet per minute. Dimensions were wingspan 27 feet 3 1/2 inches, length 31 feet 8 1/2 inches, height 10 feet 7 inches, wing area 236 square feet."