Author Topic: How would the P-38 have performed...  (Read 3969 times)

Offline Captain Virgil Hilts

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How would the P-38 have performed...
« Reply #30 on: May 06, 2006, 09:08:52 PM »
That's Widewing's site, and that P-38 is powered by F-15 Allisons.
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Offline Saxman

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How would the P-38 have performed...
« Reply #31 on: May 06, 2006, 09:30:29 PM »
Hey Kev, about props being pushed past their limits by the end of WWII...

Don't forget about the Skyraider, which continued to be developed on from Korea through Vietnam. Granted, she's an attack plane and not a fighter, but that's still impressive.
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Offline Bronk

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How would the P-38 have performed...
« Reply #32 on: May 06, 2006, 11:00:27 PM »
Quote
Originally posted by Captain Virgil Hilts
That's Widewing's site, and that P-38 is powered by F-15 Allisons.


Yea kev pointed that out for me. I skimmed it to fast.
Still an impressive test AC.



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Offline Kev367th

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How would the P-38 have performed...
« Reply #33 on: May 07, 2006, 12:13:45 AM »
Quote
Originally posted by Saxman
Hey Kev, about props being pushed past their limits by the end of WWII...

Don't forget about the Skyraider, which continued to be developed on from Korea through Vietnam. Granted, she's an attack plane and not a fighter, but that's still impressive.


Very true.
Main reason it was better for close air support to have a slower plane. (by jet standards).

Spits last combat flight was 1951, so they 'hung' on for a long time.
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Offline Saxman

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How would the P-38 have performed...
« Reply #34 on: May 07, 2006, 12:18:24 AM »
For sheer staying power you gotta give props to the F4U. First flew at the end of the 1930s and fought on with one airforce or another into the 70s.
Ron White says you can't fix stupid. I beg to differ. Stupid will usually sort itself out, it's just a matter of making sure you're not close enough to become collateral damage.

Offline Captain Virgil Hilts

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How would the P-38 have performed...
« Reply #35 on: May 07, 2006, 09:11:22 AM »
Quote
Originally posted by Widewing
Gripen and I have hashed out the P-38 quite a bit over the years, here and on usenet. Ultimately, we agree that the P-38 was a dead end in terms of development. The basic design was past mature by 1944. It was limited by a wing design that allowed for a relatively low critical Mach of just .68, whereas virtually all of its contemporaries boasted .75 through .80 Mach. At high altitude, a low critical Mach means that buffeting is as near as a lazy relative.

While many of the initial deficiencies of the P-38 were corrected over time, basic problems endemic to the design remained. Complex system controls, poor heating, generally poor outward vision, high maintenence costs, high initial purchase cost and the limitations of the wing design. All of these things conspired against the Lightning. It was competitive throughout the war, but clearly had no future beyond VJ day.

My regards,

Widewing



There's no doubt there were cheaper planes available. However, the same remains true today. An easy comparison is the F-15 and the F-16. No doubt the F-16 is cheaper and simpler. But that does not make it superior.

Lockheed certainly could have done more on the heating and on the complex controls. In fact Carlos' article on your site includes mention of the new control system Lockheed had, that, like may other things Lockheed had for the P-38, the War Production Board and the USAAC decided not to bother with.

Yes, the critical mach limit did hurt performance. But given the fact that once a prop plane enters a fight, it only gets slower, unless it dives, the critical mach limit becomes less a factor (not saying it isn't a factor at all, but just less a factor). It's a factor if you attempt to escape, or chase an escaping plane.

The basic design had limits. But the fact remains that more power and better props would have improved the performance in all areas except top speed and dive speed. Range, climb, acceleration, and turn performance would have been greatly improved. Even with maxed out Allisons and four blade Hamilton Standard High Activity paddle props, the P-38 still would not out run or out dive the fastest of the F4U, P-47, or P-51 series. But it would likely out accelerate them to 440MPH (or whatever the critical mach limit was at that particualr altitude), and it would also likely outclimb them as well as maintain speed better while climbing AND turning.

On the other hand if all you are going to do is run or dive, you aren't going to fight much. If you have to run or dive out, you've lost that fight, although admittedly you've had the ability to survive by running away. But if you cannot do anything but hope to score with a surprise high speed bounce, you don't have a truly superior plane. If you can only exhibit superior speed, and not by more than 40MPH or so, you don't have that great an edge.

Figure the average fight between prop planes begins at 360-380MPH at best, and only gets slower so long as the fight goes on, unless someone dives. Few, or more accurately, VERY few, fights began at over 400MPH, and even those were below 350MPH after the first or second turn. If you cannot out accelerate the opposing plane, you cannot even count on speed to save you after the second turn. Say the fight only drops your speed to 300MPH, you still have to out accelerate the slower plane until it can no longer accelerate. How long does it take to accelerate the faster prop planes from 300MPH to 420MPH?

The point is, had the P-38K gone into production, and the P-38 been allowed to continue to evolve with regards to engines and props (as well as the control system Lockheed already had, to name one example) it would have been far more competitive than it was to begin with, and also that it really was no more outclassed than the other prop planes after World War II ended and the jet age began. Now had the jet age NOT begun, then prop planes probably would have eclipsed the P-38 in time.
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Offline Captain Virgil Hilts

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How would the P-38 have performed...
« Reply #36 on: May 07, 2006, 09:15:43 AM »
Quote
Originally posted by Kev367th
Very true.
Main reason it was better for close air support to have a slower plane. (by jet standards).

Spits last combat flight was 1951, so they 'hung' on for a long time.


Actually, even the A-10, the best close air plane there is, is slow as well, and not much faster than some World War II era planes. And it is a jet. Probably number two, the AC-130, isn't exactly a speed demon either. By the way, it's not just to be slow, but also to have TOT, or time over target. A good close air plane has to be able to loiter long enough to be able to have a long term effect on the battle.
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Offline HoHun

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How would the P-38 have performed...
« Reply #37 on: May 07, 2006, 10:19:12 AM »
Hi Hilts,

>Yes, the critical mach limit did hurt performance. But given the fact that once a prop plane enters a fight, it only gets slower, unless it dives, the critical mach limit becomes less a factor (not saying it isn't a factor at all, but just less a factor). It's a factor if you attempt to escape, or chase an escaping plane.

High-speed controllability is a very important factor in fighter combat, offensively as defensively.

If a fighter is losing the "low-speed" fight, he can always put the nose down and run for it. If the attacker is unable to follow, he won't get the kill. In the case of the dive-speed limited aircraft being the defender, not being able to run for it is a big problem, too.

(And while it's fairly simple to dive away from two or more enemies if you enjoy a dive speed advantage, out-manoeuvring two or more enemies can be a challenge even if you enjoy a manoeuvrability advantage.)

>But it would likely out accelerate them to 440MPH (or whatever the critical mach limit was at that particualr altitude), and it would also likely outclimb them as well as maintain speed better while climbing AND turning.

The problem is that the faster you go, the shallower the possible dive angle for attacking becomes.

Von Richthofen said, "What is a fighter aircraft good for that can climb above the enemy, but then can't dive down on him to attack?"

And another disadvantage of the P-38 wing that hasn't been mentioned yet is yielded less and less lift at increasing Mach numbers. The same trend was evident for aircraft with NACA 230xx wings, like the F6F and the Fw 190, but it wasn't nearly as pronounced for these. (The P-51's laminar wing was quite good in that regard so that at high altitude, it gained in manoeuvrability compared to most other WW2 fighters.)

Pacific Theatre veteran MF Kirby once mentioned that if the Japanese had known that the P-38 was not able to follow them through a split-S, they would have have been able to escape quite frequently. Now he was flying P-38s without the dive brakes, and the Japanese pilots probably had their own reasons to avoid split-Sing, but the P-38 is still at a serious disadvantage to other Western fighters if you compare permissible Mach numbers.

Regards,

Henning (HoHun)

Offline Captain Virgil Hilts

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How would the P-38 have performed...
« Reply #38 on: May 07, 2006, 11:16:01 AM »
What made Kirby think the P-38 couldn't follow the Japanese planes? The P-38 MIGHT suffer compression issues. However, most of the Japanese planes had at least as many problems, and some more severe. Controls froze, control surfaces ripped off, and most were slower than the P-38 to begin with.

Sure the lift goes away with increasing mach numbers. I think I already acknowledged the mach limit was a problem.

The assumption that mach number is THE deciding factor is assuming too much. It simply isn't, no matter how much anyone would like it to be. The fight simply doesn't stay close to ANY plane's mach number when you're talking about piston engine prop driven planes. It just DOESN'T. Mach limit is ONE factor, and one only. PERIOD. Piston engine prop driven planes simply didn't fight at that high a speed, especially not sustained fights of any real duration.

If you can hold a turn longer and steeper, and climb better, not to mention out accelerate your enemy, why would you want to DIVE to escape him? Only a fool dives against a plane he can't out run. However, if the fight gets slow, and you are losing, if you can out accelerate and out climb your opponent, you might make a quick dive to increase your acceleration advantage and then use superior climb to escape, once you've out accelerated and gained a little separation.

Anyone who judges planes strictly on speed and critical mach is bound to be sadly disappointed in his choice before it is over with. Otherwise the fighter version of the SR-71 would be unbeatable. Yes, there was a fighter version proposed and at one time under development. By your standards, nothing on the planet could hope to defeat it. Yet it was never put into production. Why? Because ultimate speed is not the overall defining factor, even in the jet age.
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Offline HoHun

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How would the P-38 have performed...
« Reply #39 on: May 07, 2006, 11:40:59 AM »
Hi Hilts,

>What made Kirby think the P-38 couldn't follow the Japanese planes?

Well, never to split-S was an established procedure with his outfit. He once related that there were certain rules you adhered to because you had seen the guys who broke them die. I don't know whether this was one of them, but it highlights a certain amount of cautious and conservative thinking.

>Sure the lift goes away with increasing mach numbers. I think I already acknowledged the mach limit was a problem.

Well, I thought it was worth pointing out that there were ill effects even below the limiting Mach number.

>The assumption that mach number is THE deciding factor is assuming too much.

Hm, I don't think I assumed that. It's still a very important factor, though.

>The fight simply doesn't stay close to ANY plane's mach number when you're talking about piston engine prop driven planes. It just DOESN'T.

Hm, I don't think I said it does. The point is that the successful conclusion of a fight is shooting the other guy down, and that's difficult if he has the option to evade by diving. On the other hand, if you are not capable of evading by diving, that will set you up for getting shot down yourself if the fight goes bad.

>If you can hold a turn longer and steeper, and climb better, not to mention out accelerate your enemy, why would you want to DIVE to escape him?

Because he has already saddled up, coming from a position of surprise, superior numbers, superior energy, or a combination of these. You wouldn't want to dive away at the head-on merge in a 1-vs.-1, but you wouldn't want to stay in quite a lot of less fairly balanced situations.

>By your standards, nothing on the planet could hope to defeat it.

Hm, I don't think I defined any standards yet.

Regards,

Henning (HoHun)

Offline Ack-Ack

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How would the P-38 have performed...
« Reply #40 on: May 07, 2006, 01:43:12 PM »
Quote
Originally posted by Saxman
For sheer staying power you gotta give props to the F4U. First flew at the end of the 1930s and fought on with one airforce or another into the 70s.



Same for the P-38.  The P-38 flew with some airforces until the late '60s, early '70s.



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Offline Furball

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How would the P-38 have performed...
« Reply #41 on: May 07, 2006, 01:53:57 PM »
B52 has em beat :)
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Offline Ack-Ack

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How would the P-38 have performed...
« Reply #42 on: May 07, 2006, 01:59:58 PM »
Quote
Originally posted by HoHun


Pacific Theatre veteran MF Kirby once mentioned that if the Japanese had known that the P-38 was not able to follow them through a split-S, they would have have been able to escape quite frequently. Now he was flying P-38s without the dive brakes, and the Japanese pilots probably had their own reasons to avoid split-Sing, but the P-38 is still at a serious disadvantage to other Western fighters if you compare permissible Mach numbers.

Regards,

Henning (HoHun)



In McGuire's Combat Tactics For the SouthWest Pacific, he mentions that if you're jumped by Japanese planes that breaking to the right and going into a Split-S was a good defensive tactic as most Japanese planes couldn't follow.  

His manual also stated that for some reason, Japanese pilots preferred breaking to the left as opposed to the right.  Wonder why?


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Offline Furball

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How would the P-38 have performed...
« Reply #43 on: May 07, 2006, 02:04:29 PM »
torque? which way did their engines spin?
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Offline HoHun

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How would the P-38 have performed...
« Reply #44 on: May 07, 2006, 02:33:22 PM »
Hi Ack-Ack,

>In McGuire's Combat Tactics For the SouthWest Pacific, he mentions that if you're jumped by Japanese planes that breaking to the right and going into a Split-S was a good defensive tactic as most Japanese planes couldn't follow.  

Not necessarily a contradiction to what Kirby said.

In the defensve case, you would be slow, being attacked by fast Japanese aircraft. The speed picked up in a split-S would (hopefully) not suffice to bring you beyond the limiting Mach number. Being defensive, you would not be confined to track your target down, so an oblique split-S would be an option, too.

In the offensive case, you would be fast (bacause that was good tactics against Japanese aircraft), so trying to split-S would bring you to the limiting Mach number much more quickly.

(By the way, it's worth remembering that McGuire apparently was killed breaking the one rule Kirby explicitely pointed out: Not to turn with the Japanese.)

Regards,

Henning (HoHun)