 | best combination of manuverabilty and speed in an allied...| Aviation Discuss best combination of manuverabilty and speed in an allied... in the World War II - Aviation forums; Originally Posted by Erich
Gentlemen if I may add as one of the moderators on board here.
BE CIVIL !
we ... |
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01-17-2006, 04:34 PM
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#91 | | Der Crewchief
Join Date: Nov 2004 Location: Ansbach, Germany
Posts: 28,578
Country: | Quote: |
Originally Posted by Erich Gentlemen if I may add as one of the moderators on board here.
BE CIVIL !
we all come here with great expectations to learn and no-one and I mean no-one has all the answers.............
may I suggest we take more time to formulate our texts in answer and not as a mean rebuttle of words as whom are we trying to impress..........ourselves..........big deal ! there is some good and benefical information to be had here, let us not wreck this ok ?
I really do not want to see us go down a road similiar to other fourms on the net that I have had the displeasure of moderating on.
cool down, take a deep breath | Agreed!
Great info there to FBJ!
__________________ US Army Blackhawk Crewchief 2000-2006 Classic ww2aircraft.net quotes: fly boy said: "isn't that the first jet bomber? becasue i have flown one in a flight sim before and i know how it handles" "wait what ok who made the b-2 crash come on people that messed up its a b-2" "ah yes the mistel those things are so annoying is games and in real life" |
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01-17-2006, 04:50 PM
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#92 | | Senior Member
Join Date: Dec 2004 Location: Boise, Idaho
Posts: 1,178
| The P-38J-25/Ls slow speed roll rate is a bit slower than the P-51s but surpasses it at 325mph and passes the Fw-190 at about 340mph. It maxes out around 100deg/s at about 450mph (Lockheed numbers) though I've seen 110deg/sec claimed. This is aileron imput only, initial roll performance can be enhanced with throttle imput.
In '42 the P-38F was tested with all the AAF fighters ang was reported to turn as tightly (P-40) or better (P-39, P-47, P-51A) up to 15,000ft and the advantage got better as it went higher.
On the Docs page, is a test of a P-38F with 2 Spit IX's one high reduction(.477) and 1 with a lower reduction (.42) and the British decided the Spitfire could turn a little tighter but all other perameters the P-38 was in the middle between the Spitfires below 25,000ft where the Spitfire had more of an edge. They also noted a few moves the Spitfire couldn't follow effectively.
The late P-38J and L models were measurably better than the F was especialy at altitude.
wmaxt |
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01-18-2006, 12:23 PM
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#93 | | Senior Member
Join Date: Jun 2005 Location: Orange County, CA
Posts: 7,863
| Is it not true that roll rates would be different as compared between sea level and 30K?
And was there a roll rate limitation from the G forces on the pilot? It wouldnt make sense to have a fast rolling plane with a pilot blacked out as compared to slower rolling plane where the pilot is still in control.
__________________ "Pilot to copilot..... what are those mountain goats doing up here in the clouds?" |
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01-18-2006, 03:42 PM
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#94 | | Senior Member
Join Date: Dec 2004 Location: Boise, Idaho
Posts: 1,178
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Originally Posted by syscom3 Is it not true that roll rates would be different as compared between sea level and 30K?
And was there a roll rate limitation from the G forces on the pilot? It wouldnt make sense to have a fast rolling plane with a pilot blacked out as compared to slower rolling plane where the pilot is still in control. | Thats a good question and I don't know. Having said that, one is generaly going faster at altitude, at least at first, which would tighten things up a bit.
The original F4U was much faster rolling but was slowed to better balance the controls. I have also read comments from pilots that the P-38, using differential throttle to help initate a roll, could bang your head on the canopy from the abruptness but I've never heard of an aircraft rolling fast enough to black out the pilot.
I ran across some control imput info on the P-51D and P-47D at best corner speed of 300mph+/-
P-51 3g pull = 48# and a 5g pull = 86#
P-47 3g pull = 16# and a 5g pull = 27#
I don't have numbers for the P-38 just coments that rudder and elevators were great but in early models the ailerons were very high effort which is why they used a wheel instead of a stick.
wmaxt |
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01-18-2006, 04:22 PM
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#95 | | Senior Member
Join Date: Jun 2005 Location: Orange County, CA
Posts: 7,863
| [quote="wmaxt"] Quote: |
Originally Posted by syscom3 ........
I ran across some control imput info on the P-51D and P-47D at best corner speed of 300mph+/-
P-51 3g pull = 48# and a 5g pull = 86#
P-47 3g pull = 16# and a 5g pull = 27#
......wmaxt | Can you explain that a little clearer. I dont know what "48#" means.
Thanks!!!
__________________ "Pilot to copilot..... what are those mountain goats doing up here in the clouds?" |
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01-18-2006, 04:24 PM
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#96 | | Banned
Join Date: Jan 2005
Posts: 795
| # = pound(lb), so 48# = 48lb |
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01-19-2006, 11:20 AM
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#97 | | Der Crewchief
Join Date: Nov 2004 Location: Ansbach, Germany
Posts: 28,578
Country: | I would love to compare that to other aircraft such as the Spitfire, Bf-109, and Fw-190.
__________________ US Army Blackhawk Crewchief 2000-2006 Classic ww2aircraft.net quotes: fly boy said: "isn't that the first jet bomber? becasue i have flown one in a flight sim before and i know how it handles" "wait what ok who made the b-2 crash come on people that messed up its a b-2" "ah yes the mistel those things are so annoying is games and in real life" |
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01-19-2006, 02:15 PM
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#98 | | Senior Member
Join Date: Nov 2004 Location: Rising Above
Posts: 1,205
Country: | For the record:
"Don't have to be aces.
#2 in XIVs got a K-4
#401 in IXs got 4 109s
#403 in XIVs got 3 109s
#414 in IXs got 3 109s
IXs - 7, XIVs - 4
Could be more but I wasted enough time..."
If the audience takes a little time, they will see Mister KrazyKanuk wrote this before I responded in the same measure. He felt he was wasting his time and got no warning.
Case closed.
Have a lovely, a fascinating day.
*smoochies*
__________________ In a national survey, 92% of the French people believed they are not ugly: 93% of them were wrong. |
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01-19-2006, 02:21 PM
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#99 | | Senior Member
Join Date: Jun 2005 Location: Orange County, CA
Posts: 7,863
| Its interesting that the P51 has a high roll rate at high speeds. Perhaps it is better than the Spitfire at speeds above 350 knots.
Now down on the deck, I would suppose speed is what would keep you out of trouble.
What allied plane was the fastest at sea level?
__________________ "Pilot to copilot..... what are those mountain goats doing up here in the clouds?" |
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01-19-2006, 03:15 PM
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#100 | | Senior Member
Join Date: Dec 2004 Location: Boise, Idaho
Posts: 1,178
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Originally Posted by syscom3 Its interesting that the P51 has a high roll rate at high speeds. Perhaps it is better than the Spitfire at speeds above 350 knots.
Now down on the deck, I would suppose speed is what would keep you out of trouble.
What allied plane was the fastest at sea level? | Well the P-51s roll rate maxes out at about 95deg/s at ~300mph and drops to about 76deg/s at 450mph and I'm sure the effort is very high at those speeds. I think you'll find its more likely a high average rate.
wmaxt |
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01-19-2006, 03:22 PM
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#101 | | Senior Member
Join Date: Jun 2005 Location: Orange County, CA
Posts: 7,863
| "The clipped wing Spitfire has a peak roll rate of 150 degs/sec at 200 knots: it is superior to the 190 until 220 knots and then runs slightly below that until also overtaken by the P-51 at 355 knots. "
I wonder if that refers to a P51D?
__________________ "Pilot to copilot..... what are those mountain goats doing up here in the clouds?" |
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01-19-2006, 03:34 PM
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#102 | | Senior Member
Join Date: Dec 2004 Location: Boise, Idaho
Posts: 1,178
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Originally Posted by syscom3 "The clipped wing Spitfire has a peak roll rate of 150 degs/sec at 200 knots: it is superior to the 190 until 220 knots and then runs slightly below that until also overtaken by the P-51 at 355 knots. "
I wonder if that refers to a P51D? | The numbers I show for roll rate is for the P-51B. The numbers I posted for stick effort was for the P-51D model. Generaly the B model has better performance than the D but I would think the roll rate would be consistent between the two.
wmaxt |
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01-19-2006, 03:47 PM
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#103 | | Senior Member
Join Date: Apr 2005 Location: London
Posts: 2,757
| I admit that I have found this last few postings on the roll rates to be very interesting and I didn't expect the Spit to do as well as it did.
My thanks to all of you who have looked into this. Much appreciated |
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01-19-2006, 03:56 PM
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#104 | | Senior Member
Join Date: Jun 2005 Location: Orange County, CA
Posts: 7,863
| I was surprised the P47 had such low force requirements. I wonder if we can find such info for more aircraft.
__________________ "Pilot to copilot..... what are those mountain goats doing up here in the clouds?" |
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01-20-2006, 06:04 AM
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#105 | | Der Crewchief
Join Date: Nov 2004 Location: Ansbach, Germany
Posts: 28,578
Country: | That is what I am researching right now. Probably wont have anything till next week though, because I wont have much time this weekend.
__________________ US Army Blackhawk Crewchief 2000-2006 Classic ww2aircraft.net quotes: fly boy said: "isn't that the first jet bomber? becasue i have flown one in a flight sim before and i know how it handles" "wait what ok who made the b-2 crash come on people that messed up its a b-2" "ah yes the mistel those things are so annoying is games and in real life" |
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