In keeping with my usual practice, I took the newest additions to the plane-set offline to quantify performance.
I did speed runs at MIL power and WEP at sea level (50 feet) and 5,000 feet.
I did max climb from sea level to 5,000 feet
I did minimum turn radius without flaps and with full flaps.
I also did max dive speed before failure, unloaded (no g applied to airframe).
All data was taken at 25% fuel at zero burn rate (about 28 minutes of gas in the MA) and no bombs.
Here's the data....
SPEED-
Sea level max speed, MIL power:
B-25C glass nose: 265 mph
B-25C solid nose: 264 mph
B-25H: 263 mph
Sea level max speed, WEP power:
B-25C glass nose: 277 mph
B-25C solid nose: 276 mph
B-25H: 274 mph
5,000 feet max speed, MIL power:
B-25C glass nose: 283 mph
B-25C solid nose: 282 mph
B-25H: 281 mph
5,000 feet max speed, WEP power:
B-25C glass nose: 293 mph
B-25C solid nose: 292 mph
B-25H: 291 mph
Max dive speed before structural failure (zero g loading): 450 mph
Max speed to induce structural failure at 4 g loading: 355 mph
Notes: Lighter weight means a slight increase in speed, but there is little to choose from as spread is typically just 3 mph from fastest to slowest. However, the B-25H has the slowest acceleration, typically taking 10 seconds longer from 200 to 250 mph. This is expected, because it is the heaviest of the three.
CLIMB-
Climb from sea level to 5,000 feet, beginning at 160 mph, using WEP power. Time in minutes:seconds.tenths of seconds to reach 5k.
B-25C glass nose: 2:04.70
B-25C solid nose: 2:13.59
B-25H: 2:29.81
TURN RADIUS-
B-25C glass nose not tested, but should be a bit better than B-25C solid nose.
Full flaps, three turns counter-clock wise, average time and speed. Three tests done, results averaged.
B-25C Solid nose: 705.7 feet @ 12.62 degrees/sec
B-25H: 772.1 feet @ 12.13 degrees/sec
No Flaps, B-25C solid nose tested: 837.0 feet @ 16.17 degrees/sec.
Max speed that allows you to begin lowering flaps is 185 mph IAS.
Note: Weight makes a big difference here. Considering the size of the aircraft, the turn radius is excellent. However, the turn rate is appallingly slow. Using flaps to maneuver with other aircraft, especially fighters is generally counter-productive. While you may gain an angle for a snap shot, you will find yourself hopelessly slow with little prospect of regaining E over the short term.
I suggest not using flaps while turning with other aircraft. Take note that the B-25C (solid nose) turns very well without flaps beginning from 260 mph. Be sure to trim manually, with elevator trim neutral (mid scale on the indicator). Starting at 260 mph, the B-25C can complete a 360 degree turn in 19.9 seconds, averaging just over 18 degrees a second. Since it bleeds E rapidly, the turn tightens dramatically. Clean and devoid of bombs, it turns tighter over one circle than a Fw 190D-9 or the A-8, and at a comparable rate of turn too. Of course, the B-25 bleeds E like crazy, and will not be able to sustain this much beyond a single circle, thus the 190s will quickly reverse the table on the Mitchell. Nonetheless, the B-25's excellent instantaneous turn rate and its tremendous gun package means that it is a major threat to many fighters during the first stages of a fight. You must make the first opportunity count as there is a strong possibility that there will not be a second chance, unless the enemy pilot is hopelessly inept (fortunately, there's plenty of those).
Speaking of manual trim, if attacking ground targets, be sure to trim at least neutral elevator to prevent augers. DO NOT load the aircraft beyond 4 g in the pull out. DO NOT trim so much up elevator that it induces more than 4 g. Reduce power to idle and attempt not to exceed 300 mph when diving on ground targets.
I forgot this myself and clipped a tree while carrying 2 fighter kills and 3 GV kills... Wasn't happy with my oversight.
My regards,
Widewing