Originally posted by Widewing
Careful? Too careful, I think.
50% fuel, full ammo, max power (WEP) . . .
It's good that you did the test, but I was using full power, not war-emergency power. Under my stated conditions, I'd be interested to know what numbers you get. I did a test with WEP turned on. What I get is below. Are you sure you are getting to steady state before starting the timing of your three turns? In other words, are you doing 5 or more stall turns before you start timing your 3? If so, can you send me a film of one of your runs? -- I'd be very curious why you and I, supposedly doing the same test, are getting different numbers (brooke at electraforge.com). My numbers below are repeatable to within a second or two, and I am flying to edge of the snap-spin/stall.
FW 190A-8, 64 sec
P-47D-25, 67 sec
P-47D-25 (1notch), 65 sec
Originally posted by Widewing
Both the P-47 and P-51 can deploy one notch of flaps at 400 mph, meaning that the Fws will find themselves even further behind the 8-ball.
Beyond the speed at which you are pulling max g's (which limits the g's you can pull to a constant), turn rate is just a function of airspeed -- nothing else. Dropping a notch of flaps there is just acting like air brakes, scrubbing off speed. You can dump energy and tighten the turn until you run out of airspeed through any number of techniques: a notch of flaps, speed brakes, chopping throttle, or possibly standing on rudder. This is just a transient effect.
Originally posted by Widewing
By the way, the P-38L rolls faster than the Fw 190 above 350 mph, with the difference becoming larger as speed goes up.
I just tested the P-38L vs. the FW 190A-8 at 10k altitude at about 375-400 mph indicated, holding a shallow dive to hold the speed in that range. The P-38L does 3 rolls in 10.5 seconds. The FW 190A-8 does 3 rolls in 10.5 seconds. Above about 400 mph at 10k and higher, the P-38L starts to hit compressibility. Much inside compressibility, it's roll rate goes to crap. The FW 190A-8 hits compressiblity there at about 500 mph indicated. So, in roll rate, the P-38L gets trounced by the FW 190A-8 all the way up to moderate speeds, the P-38L draws to parity (but not superiority) at a narrow range of high speeds, then gets trounced again above that range. So, I'd still say the FW 190A-8 is much better at roll.
Originally posted by Widewing
Wilbus is correct, the 190A-8 will not out-turn any P-47 (especially the D-11) even without the P-47 using flaps. However, using flaps in the Jug allows it to gain a significant edge.
I disagree that the P-47D has a significant advantage over the FW 190A-8 in stall-turn performance. I believe that the FW 190A-8 is in fact better (although not by a huge amount). I'd be willing to go on-line in the dueling area together to check it out.
Getting back to what points I am trying to make:
1. The US planes are not uniformly better at maneuvering than the German ones.
2. The P-47D is not a great-turning plane and does not handily outturn a FW 190.
3. I doubt HTC biases the modelling in favor of US planes.