Author Topic: p51b vs p51d  (Read 7113 times)

Offline Lusche

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p51b vs p51d
« Reply #75 on: February 14, 2007, 12:58:57 PM »
Quote
Originally posted by Benny Moore
I'm with Bronk.  The F4U Corsair can do everything the P-51 can do and a lot more.  It's faster, climbs better, accelerates better, and turns better.


Only the F4U-4. The P51D is faster & has a better climbrate than all the other hogs (but of course, it turns much worse)
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Offline Krusty

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« Reply #76 on: February 14, 2007, 01:02:00 PM »
Quote
Originally posted by Benny Moore
It's faster, climbs better, accelerates better, and turns better.


No, no, no, and yes.

I had a feeling this wasn't the case (from personal experience in both sets of planes) and checked. Quite interesting. The f4u definitely has an edge in flaps and gear and handling and ammo load, but the p51s are faster and climb better and acceleration is about even.

http://www.gonzoville.com/ahcharts/index.php?p1=f4u1&p2=f4u1d&p3=p51b&p4=p51d

Offline Bronk

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« Reply #77 on: February 14, 2007, 01:16:41 PM »
Just to clarify all I'm saying is the hog can play the E game just as effective as the  mustang. Not climb better, accelerate or faster. It makes up for these in zoom, dive and roll.

Now lets see a 51 dump e faster than a hog, and float around as well full flap low and slow.

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Offline Benny Moore

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« Reply #78 on: February 14, 2007, 05:11:33 PM »
Check the Dash Four, Krusty.  By the way, while doing some figures for another set of ships, I noticed that while dropping flaps cut turn radii by about 27% on many ships (P-38, P-47, Me-109, FW-190, Ki-84, and even the La-7), the F-4U Corsair gets its turn radius cut by a whopping 40%.  The P-51, on the other hand, only obtains a 21% cut.

I wonder what it is about those first six ships which causes them all to have the same approximate fraction of their turning circle removed with flaps (especially interesting since the P-38 and Ki-84 had Fowler flaps).  Moreover, I wonder what it is about the Corsair that causes it to do so much better in this.  It's not as if it had Fowler flaps or anything special.
« Last Edit: February 14, 2007, 05:14:36 PM by Benny Moore »

Offline Ack-Ack

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« Reply #79 on: February 14, 2007, 05:19:19 PM »
Quote
Originally posted by Hades55


It takes more skills to fight (and win) flying a pony than a f4u or f6.

 



Every plane takes skill to be able to fight successfully in.  


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Offline Krusty

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« Reply #80 on: February 14, 2007, 06:13:28 PM »
When most folks say "the F4u" they don't mean the -4. It's the exception to the rule, and is perked for a good reason.

All versions except the -4 are inferior in climb and speed, and only match the acceleration of the p51s.

Offline Widewing

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« Reply #81 on: February 14, 2007, 06:32:33 PM »
I was working with a guy who flies the P-47s as his MA ride.  He's been going through a flat spot (all pilots hit these bumps in the virtual road from time to time) and wanted to work on his ACM. We began flying the P-47D-11. After an few duels, I took a D-25 trying to even out things a bit as he was struggling some. Not even enough. So, I grabbed a P-51D.

If I flew a pure E fight, the P-51D was perfectly adequate. However, if I dumped flaps and maneuvered, the Mustang was badly outclassed by the D-11. I switched to the P-51B and there was little improvement.

This was really bothering me. Flaps out, the P-51s are absolute pigs. Indeed, the P-51B has a turn radius that is nearly 70 feet greater than the P-47D-11.

Consider that a low fuel P-51B (25% gas) weighs right around 9,000 lb and the P-47D-11 (25% gas) weighs about 12,200 lb.

This results in respective wing loadings of:
P-51B: 38.59 lb per sq/ft
P-47D-11: 40.66 lb per sq/ft

Even with flaps up, the P-47D-11 out-turns the P-51B. That simply should not be the case.

P-51s and P-47s have a similar maximum coefficient of lift.
P-51B: 1.89
P-47D: 1.93

If we take the wingloading and divide it by the co-efficient of lift, we have a reference indicator of turning ability.

So, for the P-51B: 38.59/1.89 = 20.42
For the P-47D-11: 40.66/1.93 = 21.07
Thus, the P-47's turn radius should be 103% of that of the P-51B (clean, no flaps).

Unfortunately, in the game it's backwards.
P-51B turn radius, clean: 758.2 feet
P-47D-11 radius, clean: 748.4 feet
Thus, the P-51B's turn radius is 101.3% of that of the P-47D-11.

So, in AH2, the P-47D-11 turns slightly smaller circles than the P-51B. Adding flaps in increments results in the P-47 gradually turning smaller circles until at full flaps, the difference in just short of 70 feet. This results in the P-51B turn radius being 113% of that of the P-47D-11.

From: wwiiaircraftperformance.org


BRIEF TACTICAL COMPARISON WITH SPITFIRE XIV

Maximum Endurance
25. By comparison the Spitfire XIV has no endurance.

Maximum speed
26. There is practically nothing to choose in maximum speed.

Maximum climb
27. The Spitfire XIV is very much better.

Dive
28. As for the Spitfire IX. The Mustang pulls away; but less markedly.

Turning Circle
29. The Spitfire XIV is better.

Rate of Roll
30. Advantage tends to be with the Spitfire XIV.

Conclusion
31. With the exception of endurance, no conclusions should be drawn, as these two aircraft should never be enemies. The choice is a matter of taste.

BRIEF TACTICAL COMPARISON WITH TEMPEST V
Maximum endurance
32. By comparison, the Tempest V has no endurance.

Maximum speed
33. The Tempest V is 15-20mph faster up to 15,000ft. There is then no choice until 24,000ft when the Mustang rapidly pulls ahead, being about 30mph faster at 30,000ft.

Maximum climb
34. These compare directly with the results of the speed tests. At similar performance height, the Tempest has the better zoom climb.

Dive
35. The Tempest tends to pull away.

Turning circle
36. The Tempest is not quite as good.

Rate of Roll
37. The Tempest is not so good. This attribute of the Tempest V may be improved upon in later aircraft.

Conclusions
38. The Mustang has endurance and general performance above 24,000ft. Conclusions should not be drawn below this height, but the Tempest has a better speed and climb below 10,000ft.


Note that the AH2 Tempest out-turns both the P-47D-11 and the P-51B...

When the drag model was revised, the P-51s suffered a large hit to their turn radius, especially with flaps out. They went from reasonably capable to absolutely helpless in an instant. Only the Fw 190A-8 and F-8 have  larger turn radii than the P-51D.

This is another thing that needs to be looked at. Our P-51s have lost much of their luster. I'm hoping that HTC looks at them again before Combat Tour debuts.

My regards,

Widewing
My regards,

Widewing

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Offline 1K3

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« Reply #82 on: February 14, 2007, 07:52:21 PM »
Quote
Originally posted by Widewing
Our P-51s have lost much of their luster. I'm hoping that HTC looks at them again before Combat Tour debuts.


Nah the '51s feels alright this time.  

Last year (or 2) you can pretty much outturn many planes at very slow speeds (even the spit) with '51s wonder flaps (TM), which is downright and outright B.S.

Offline Bronk

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« Reply #83 on: February 14, 2007, 08:00:46 PM »
Quote
Originally posted by 1K3
Nah the '51s feels alright this time.  

Last year (or 2) you can pretty much outturn many planes at very slow speeds (even the spit) with '51s wonder flaps (TM), which is downright and outright B.S.


Please post your data/flight logs to back this up.


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Offline Treize69

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« Reply #84 on: February 14, 2007, 09:35:56 PM »
Yeah, even before the revision we used to outturn Ponies in 109s at most altitudes in the AvA. Its gotten worse now, but its by no means gone from being totally uber to useless.

btw, I never use flaps to turn, so I can't offer an opinion on performance there.
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Offline Widewing

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« Reply #85 on: February 15, 2007, 05:15:24 AM »
Quote
Originally posted by 1K3
Nah the '51s feels alright this time.  

Last year (or 2) you can pretty much outturn many planes at very slow speeds (even the spit) with '51s wonder flaps (TM), which is downright and outright B.S.


Even if I believed you had some basic understanding of what I've discussed, I'd still label your post as baloney.

At their best, when AH2 was first released, P-51s could not out-turn Spitfires. Not even close. At best, they could almost almost turn with a Spitfire XIV when using full flaps. The current modeling is substantially different, with the P-51D only able to out-turn the 190A-8, 190F-8 and the Me 262. It is inferior to every other fighter. In the real world, that simply was not the case.

When the drag modeling was changed (at the time that the revised Bf 109s were introduced), the P-51 was adversely affected more than any other fighter.

These are indisputable facts:

P-51s had a lower wingloading than P-47s at normal combat weights. P-51s had a nearly identical coefficient of lift to that of the P-47.

Thus, P-51s should have smaller turning circles than all of the P-47s. The Brits certainly thought that this was the case.



My regards,

Widewing
My regards,

Widewing

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Offline Benny Moore

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« Reply #86 on: February 15, 2007, 07:43:28 AM »
So did the American P-51 pilots.  The father of one of my old squadron members flew P-51s as a gunnery instructor, and his words were "turns almost as good as a Spitfire."  Since the P-51's the worst turning fighter in the game barring the FW-190, that statement cannot possibly be made with any credibilty of the P-51 in Aces High II.

Offline whiteman

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« Reply #87 on: August 22, 2007, 05:46:02 PM »
glad i looked this up, think i found some usefull info. I've been in the 51d as of late and i'm just dead meat flying around in that thing. I tried the B was worried about the guns and landed 4 kills first time. only reason i have to fly the D is the veiw and extra guns.

Offline Charge

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« Reply #88 on: August 23, 2007, 03:12:53 PM »
Extract from WW2aircraft.net:

Bf 109K-4 Aerodynamic statistics:

Wing-loading *Loaded*: 191.9 kg/sq.m. (39.2 lbs/sq.ft.)
Wing Aspect-Ratio: 6.06 .
Airfoil: NACA 2R1 14.2 - 2R1 11.35.
Airfoil Thickness Ratio: Root= 14.2% Tip= 11.35%.
Wing CL-max *Freeflow*: 1.48 . (No slats or flaps deployed)

Lift-loading *Loaded*: 129.69 kg/sq.m. (26.5 lbs/sq.ft.)
Power-loading *Loaded*: 1.57 kg/hp. (3.47 lbs/hp.)


P-51D Mustang Aerodynamic statistics:

Wing-Loading *Loaded*: 196.33 kg/sq.m. (40.5 lbs/sq.ft.)
Wing Aspect-Ratio: 5.81 .
Airfoil: "Laminar" NAA/NACA 45-100 - NAA/NACA 45-100.
Airfoil Thickness Ratio: Root= 14.8 or 15% Tip= 12%.
Wing CL-max *Freeflow*: 1.28 . (No flaps deployed)

Lift-loading *Loaded*: 153.38 kg/sq.m. (31.6 lbs/sq.ft.)
Power-loading *Loaded*: 2.49 kg/hp. ( 5.49 lbs/hp.)

Wing Cl-max were obtained from:

Bf-109: from full scale Windtunnel test in Charlais Meudan.
P-51: from Naca Report 829, Page 26 in the PDF of the Naca Report server.


:huh


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Offline Sable

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« Reply #89 on: August 23, 2007, 06:23:57 PM »
Worth noting is that the aircraft being measured in NACA report 829 is a P-51B, and the 1.28 CLmax value is for the aircraft with no propellor and it's gun ports open.  Units often did cover these ports with tape to clean up the wing.  In the report it lists the CLmax at 1.39 with them covered.  Interestingly NACA also tested the aircraft with 3/4" holes drilled in their covers to allow for the guns to fire, and got a result of 1.37.  Would shot through tape with a 1/2" hole perform better or worse?  Who knows.



This shot shows a 4th FG P-51B with the gun ports taped.

Interestingly the P-51D wing had a much different design for the gun ports.  The openings were smaller and faired, and often still taped by ground crews.



This is a 364th FG P-51D with it's gun fairings taped.  Both photos came from http://www.web-birds.com.

As a reference point, the report also gives the CLmax of an F4U-1 Corsair, in the same service condition (open gun ports etc) as the P-51 as a mere 1.17!  An F6F recorded a 1.28-1.29 in service condition.  They also mention in the report that flying aircraft with turning propellors would return higher values then static aircraft in their wind tunnel, so YMMV.