Author Topic: P-38l  (Read 4270 times)

Offline Captain Virgil Hilts

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« Reply #30 on: May 04, 2004, 07:45:46 AM »
Quote
Originally posted by HoHun
Hi Hilts,

>No, actually, if the pilots said they could and did follow their enemy right on through a split S into a dive and catch them, and YOU say they didn't, and they couldn't, I'd say it is your word against theirs.

You are a liar, Hilts.

You either come up with a direct, unambigous quote proving your claim, or I'll report the next post where you make an unfounded claim like that to the moderation of this forum, complete with a request to take action against you.

Henning (HoHun)


Do it Hohun, run tell your mommy. I'm sure they'll get all bent over it.

(note: The above statement is in no way a sign of a lack of respect for Skuzzy. But I really doubt Skuzzy would need me to say that, I'm sure he actually understands quite well what I meant. I think it would be rather sad and pitiful for someone to go and complain to Skuzzy over this thread.)

Oh, and while you are at it Hohun, here:

"Nothing, to these pilots, after the hard winter of 1943-44 could be more beautiful than a P-38L outrolling and tailgating a German fighter straight down, following a spin or split-S or whatever gyration a startled, panicked and doomed German might attempt to initiate. You just couldn't get away from the P-38L. Whatever the German could do, the American in the P-38L could do better." (cited from [8] with permission from Arthur W. Heiden).

Now, go ahead and call Captain Arthur Heiden, pilot of "Lucky Lady" of the 79TH FS of the 20TH FG a liar. Go ahead, I don't care anymore Hohun, I really don't. And go report me to the moderator, ooooh ooooh, I'm so scared.

(see note above)

Now we see who the liar is. If you can't handle the truth from a fighter pilot who was there, well ain't that just tough.
« Last Edit: May 04, 2004, 09:04:44 AM by Captain Virgil Hilts »
"I haven't seen Berlin yet, from the ground or the air, and I plan on doing both, BEFORE the war is over."

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Offline Captain Virgil Hilts

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« Reply #31 on: May 04, 2004, 07:49:08 AM »
Quote
Originally posted by DiabloTX
I remember seeing or reading an anecdote by a 38 pilot that claimed he could turn inside *any* LW plane by simply cutting the throttle to the engine on the side he was turning into.  I will look for this source and post it but I remember him saying that in the right hands the 38 was more than a match for LW iron.

G, those quotes you posted, they are all about new squads getting hosed.  How about some quotes from 38 squads that were veterans?  I for one would like to see them.

Thanks.


This is all I have time for bud, don't wait around for them to tell you the truth and find quotes from BOTH sides, you'll be long dead before it happens. But here you go, from an article by Dr. Carlo Kopp, written with help from two guys I know who were P-38 pilots: http://home.att.net/~ww2aviation/P-38.html

See also those sites listed above. Those are almost all run by the associations of their respective groups and squadrons. With quotes from their pilots and leaders, and lists of their aces.

Of course, do not be at all surprised if you hear that they were liars, and nothing you read on the Internet can be trusted.
« Last Edit: May 04, 2004, 08:14:51 AM by Captain Virgil Hilts »
"I haven't seen Berlin yet, from the ground or the air, and I plan on doing both, BEFORE the war is over."

SaVaGe


Offline straffo

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« Reply #32 on: May 04, 2004, 07:50:30 AM »
Quote
Originally posted by GScholz
The fact still remains that the P-38’s service was unsatisfactory and was largely withdrawn from fighter service in the ETO when the P-51 became available in numbers.  


There is probably some other reasons like cost and maintenance.

Offline Captain Virgil Hilts

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« Reply #33 on: May 04, 2004, 07:51:07 AM »
Quote
Originally posted by DiabloTX
Ouch.  I was just hoping with your vast amount of anecdotal and data facts that you could post some rather quickly.  I was not meaning anything argumentative or debatable about my request.  Since you seem to have taken it the wrong way I retract my request, as small as it was, and will leave this debate to the "experts" who seem to be taking it way too personally.


Don't be surprised by this, it is the normal response. See the post above where I replied to your request. It is all there, you just have to do a little research. Look to those websites I posted earlier as well.
"I haven't seen Berlin yet, from the ground or the air, and I plan on doing both, BEFORE the war is over."

SaVaGe


Offline Captain Virgil Hilts

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« Reply #34 on: May 04, 2004, 07:57:57 AM »
Quote
Originally posted by straffo
There is probably some other reasons like cost and maintenance.


Exactly. The P-38 cost $125K each. They required about 30% more maintenance. They required a completely different set of supplies. They required completely seperate training. They were VERY hard to get as only Lockheed was making them, and only in one plant which was over half devoted to B-17 production. Units elsewhere were begging for them. The 8TH AF until the time Doolittle took over had no idea what to do with long range fighter aircraft. The results of the inadequacies of the 8TH AF staff officers and leadership was blamed on the P-38.

The 5TH AF wanted all the P-38s they could get, since the P-38 was being properly used there to kill more Japanese planes than all other fighter aircraft in the theatre. They knew how to use the P-38 and how to run an Air Force. Pilots there were racking up kills at an astounding rate. Pilots who came from the European theatre for the most part said the Japanese were a more dangerous foe than the germans.
"I haven't seen Berlin yet, from the ground or the air, and I plan on doing both, BEFORE the war is over."

SaVaGe


Offline Captain Virgil Hilts

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« Reply #35 on: May 04, 2004, 08:12:59 AM »
Look at the performance numbers and pilot reports from those who flew the P-38 and you may find it is not overmodeled, nor is it in the "easy mode".

It was remarkably stable, to a fault if you consider how hard it was to get it to roll at times. It had the best manners of any fighter simply because it had two engines and two props that rotated in opposite directions like huge gyroscopic stabilizers. It had a high aspect ratio wing and Fowler flaps for lift and handling. It had a combined HP of over 3200, spread through two props for better utilization of available power. It had turbochargers to retain maximum performance from sea level to well over 30K feet. It concentrated its gunfire in a 30" circle from 1 foot to more than 1500 feet from the muzzles. It had a hard hitting 20mm cannon with 150 rounds, and four 50 BMGs with 500 rounds each. It had great acceleration in level flight and in a dive, a relatively high top speed, an excellent climb rate, excellent range, good handling at both low and high speeds, especially later models with hydraulic assist ailerons and dive flaps.

On the otherhand, it could not get much over 500 MPH in a dive, and it was very hard to handle in a dive at higher speeds and altitudes. It had very poor cockpit heating. Early models had poor intercoolers and weak electrical systems, amnd not as much internal fuel capacity. It was very complex and had nearly double the controls for the engines and props. The fuel system was difficult to manage unless you looked right at the switches, and even then they were hard to operate with gloves on. The engines had little if any automatic management, at least in the early models. It required special training to get the most power and the most fuel efficiency, not to mention the best handling. It had pooor visibility compared to many fighters.
"I haven't seen Berlin yet, from the ground or the air, and I plan on doing both, BEFORE the war is over."

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Offline GScholz

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« Reply #36 on: May 04, 2004, 08:28:24 AM »
Quote
Originally posted by DiabloTX
Ouch.  I was just hoping with your vast amount of anecdotal and data facts that you could post some rather quickly.  I was not meaning anything argumentative or debatable about my request.  Since you seem to have taken it the wrong way I retract my request, as small as it was, and will leave this debate to the "experts" who seem to be taking it way too personally.


I did not mean to insult you in any way, I apologize if I did. :confused:
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Offline Captain Virgil Hilts

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« Reply #37 on: May 04, 2004, 08:45:54 AM »
Quote
Originally posted by GScholz
I did not mean to insult you in any way, I apologize if I did. :confused:


Very big of you to apologize to him Scholz.  I can respect that.
« Last Edit: May 04, 2004, 08:54:54 AM by Captain Virgil Hilts »
"I haven't seen Berlin yet, from the ground or the air, and I plan on doing both, BEFORE the war is over."

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Offline Captain Virgil Hilts

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« Reply #38 on: May 04, 2004, 08:54:30 AM »
This has begun to take far too much of my time. I've far better things to do. I'm wasting time here I could spend flying and improving my woefully inadequate skills and talents. You guys can have it. No amount of arguement will change anyone's position.
"I haven't seen Berlin yet, from the ground or the air, and I plan on doing both, BEFORE the war is over."

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Offline GScholz

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« Reply #39 on: May 04, 2004, 09:34:12 AM »
Quote
Originally posted by Captain Virgil Hilts
Look at the performance numbers and pilot reports from those who flew the P-38 and you may find it is not overmodeled, nor is it in the "easy mode".


EVERY plane in AH is "easy mode" compared to the real thing. If you don't understand that then you are beyond reason. NONE of the P-38's nasty compressibility problems are modelled, you don't really need the dive brake in AH since you can trim all planes out of compressed dives. In AH the only thing that happens is that the controls stiffen up. In real life it was a lot worse:

Quote
Compressibility occurs when the P-38 entered dives stated above 20,000 ft. The airflow would be "splashed" over the leading edge of the wing instead of the usual smooth airflow. The splashed air would approach the sound barrier (not the aircraft itself, but rather the speed of the air flowing over the wing), thus causing a shockwave effect on the trailing edge. This would render the controls inoperable, leaving the pilot without any control of the aircraft. Two possibilities would then ensue. Either the aircraft would slow as it descended into denser air closer to the ground and the pilot would regain control and pull out of the dive. Or in some cases, the P-38 would simply disintegrate. Many pilots would lose their lives when they inadvertently entered a steep dive, or when performing dive tests.


Tony Levier described compressibility as, "It resembled a giant phantom hand that seized the plane and sometimes shook it out of the pilot's control." George Gray wrote in a history of the NACA, "The behavior was new to pilots, terrifying, baffling. Several men, in putting this two-engine fighter through its diving maneuvers, underwent the experience: A sudden violent buffeting of the tail accompanied by a lunging and threshing about of the place, as though it were trying to free itself on invisible bonds, and then the maddening immobility of the controls, the refusal of the elevators to respond to the stick." Use of elevator trim would sometimes bring the P-38 out of a dive before destruction. Sometimes the P-38 would begin to tuck under and begin to come out of the dive upside-down. Levels of stress on the airframe were staggering.


Would you like this behaviour modelled if you forget to deploy your dive brakes? Didn't think so.


And the link you posted corroborates my point of view that the P-38 was unsuited for operation in the ETO and was unsuccessful in the fighter role:

Quote
With a large proportion of Pacific and Med P-38 operations flown at medium to low altitudes, Lockheed and Allison had little operational experience with the aircraft at high altitude and low ambients and this was quickly revealed. The Allisons misbehaved quite consistently, 'throwing rods, swallowing valves and fouling plugs' while the intercoolers often ruptured under sustained high boost, and turbocharger regulators froze at 10 in. or 80 in. of boost, the latter often resulting in catastrophic failures. Even with the arrival of the P-38J, engines and turbochargers continued to fail. The new intercooler/oil cooler design was actually too efficient and the enlarged radiators became a new problem. Fuel too, was a source of trouble, it is believed by many knowledgeable people that the majority of fuel used in Britain was improperly blended, the anti-knock lead compounds coming out of solution (separating) in the Allison's induction system at extreme low temperatures. This could lead to detonation and rapid engine failure, especially at the higher power settings demanded for combat.


Quote
To aggravate these problems, inadequate cockpit heating resulted in severe pilot frostbite, while the Luftwaffe quickly learned about the compressibility problems in dives, with German pilots evading the P-38s by executing a split-S at high speed. The initial roll rate was not spectacular and the easily recognized planform provided the Luftwaffe with yet another advantage to play.

Poor serviceability and engine problems meant that initially 50 or less aircraft were available for such missions, including the first escorts over Berlin, and therefore the 55th and later also 20th FG usually fought the JGs outnumbered between three to one and five to one, as noted previously. The large number of engine failures deep inside enemy airspace exacerbated the problem, and the aggregate exchange rate, accidents inclusive, dropped to about 1:1.5 in favour of the Lightning by 1944. Aircrew morale dropped, moreso due to the large number of single engine landing accidents, thus further damaging the aircraft's reputation. The technical problems were not resolved until the introduction of the P-38J-25-LO, by which time the 8th had decided that the new Merlin powered P-51B/C was a better choice for the mission.


The LW fighters could disengage at will, and a 1:1.5 loss ratio against the LW when they were concentrating on the bombers ... not very impressive compared to the P-47 and P-51.


Quote
Despite these difficulties the 55th did well on a number of sorties during this period. On the 3rd November, 1943, the 55th in concert with the experienced 4th, 56th and 78th FGs clashed with the elite JG 1. The 55th accounted for 7 Luftwaffe fighters of the 13 claimed. On the 25th November, 1943, 4 FW-190s were claimed for the loss of one P-38H, one of the Focke-Wulfs belonging to Major J. Seifert (an "expert" with 57 kills), Gruppenkommandeur of II/JG26. Other sorties were much less successful, and heavy losses were suffered on a number of occasions.



Of course there are pilot quotes like these:

Quote
"Nothing, to these pilots, after the hard winter of 1943-44 could be more beautiful than a P-38L outrolling and tailgating a German fighter straight down, following a spin or split-S or whatever gyration a startled, panicked and doomed German might attempt to initiate. You just couldn't get away from the P-38L. Whatever the German could do, the American in the P-38L could do better."


Quote
"The P-38J25-LO and P-38L's were terrific. Roll Rate? Ha! Nothing would roll faster. The dive recovery flaps ameliorated the "compressibility" (Mach limitation) of earlier Lightnings. An added benefit of the dive recovery flaps was their ability to pitch the nose 10-20 degrees "up" momentarily when trying to out turn the Luftwaffe's best, even when using the flap combat position on the selector. Of course the nose "pitch-up" resulted in increased aerodynamic drag, and must be used cautiously. High speed is generally preferred over low speed in combat situations. Properly flown, the Fowler flaps of the P-38 allowed very tight turning radius."



Rather nice quotes from pilots who obviously liked the P-38L, however the " You just couldn't get away from the P-38L. Whatever the German could do, the American in the P-38L could do better" and the "Roll Rate? Ha! Nothing would roll faster" should be taken as enthusiastic boasting common to all pilots.


This quote is far more telling of the P-38 experience in the ETO:

Quote
"The P-38 was a large fighter with much mass. 52' wingspan and long, wide-chord ailerons contributed to slow response along the longitudinal axis of the early airplanes. The higher the indicated airspeed, the slower the response. At very high IAS it took plenty of muscle to roll the airplane. I don't believe that a joystick would have improved matters over the wheel. The Luftwaffe soon recognized the slow roll rate of the "H" and early "J" model Lightnings and used it to their advantage. It also learned of the dive restrictions caused by "compressibility" and used that advantage also.

Sometime in the development of the P-38, the design engineers must have realized that P-38's didn't have great roll capability. When Tony Levier, Lockheed test pilot, visited the 55th FG, he heard a common thread of complaints from the pilots. Cold cockpit, poor "flick" roll rate, and inability to dive after the Bf-109's and FW-190's from high altitude.


The P-38L did not enter service until June 1944. At that time the LW had long since lost the air war and apart from a few Experten, fielded nothing but inexperienced pilots whom were facing daunting numerical odds. Any statistics from this period of the war is more or less useless. Anecdotal evidence from the few LW pilots that survived the war suggests that they had little problem with the P-38 and P-47 ... it was the P-51 they had trouble beating.


Quote
Originally posted by Captain Virgil Hilts
This has begun to take far too much of my time. I've far better things to do. I'm wasting time here I could spend flying and improving my woefully inadequate skills and talents. You guys can have it. No amount of arguement will change anyone's position.


Doh! So I've written all this for nothing? ;)

I'm sure your skills will improve to the point of loving the AH P-38 as much as you love the real (or perceived real ;)) one. Ask Ack-Ack to let you in on his secrets ... on second thought don't! Having one Ack-Ack in the MA is enough for me to get jumpy when I see a knit 38. Good luck in the MA.
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Offline GScholz

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« Reply #40 on: May 04, 2004, 10:23:45 AM »
Quote
Originally posted by DiabloTX
How about some quotes from 38 squads that were veterans?  I for one would like to see them.


Quote
Originally posted by GScholz
Why don’t you find some quotes? If you can find them (I’m sure you can).


I see now how this could be interpreted as an insult. I did not mean to imply that you are incapable of finding quotes. I meant that it perhaps would be difficult to find quotes from P-38 veterans from that time in the war. My English is sometimes not as good as I'd like it to be. I'm sorry for the ambiguity of my post.
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Offline MiloMorai

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« Reply #41 on: May 04, 2004, 10:25:00 AM »
If this link has not been posted already, it is well worth the read.

http://www.yarchive.net/mil/p38.html

Offline bozon

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« Reply #42 on: May 04, 2004, 10:31:03 AM »
In RL high altitue fighting wasn't so spectacular. Almost all the accounts I've read (apart from very rare 1on1 fights) describe "dweebish" flying with almost no ACM involved save the "split-S and dive".

Up high, climb-rate is near useless while diving ability is almost everything - this is the biggest problem the 38s faced, and the dive-flaps didn't help a lot. It did help by allowing pilots to dive the 38 safly untill hitting the edge of the envelop AND pull out of the dive. With out this confidence I'm sure most of them didn't exploit the (limited) dive ability to it's fullest. L model or not, this was always the greatest disadvantage.

on the other hand, mid-low altitudes, there's not much room for dives and a great use for climbs. The 38 could really excell there and did. Plus, it's range often made it the only usable plane (PTO).

It simply wasn't a high alt plane and not fit for high alt bomber escort. But it was the only option for a long time.

this is my OPINION of the matter.

Bozon
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Offline MiloMorai

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« Reply #43 on: May 04, 2004, 10:40:57 AM »
One must remember that a diving LW a/c is out of the 'fight'. There was no fuel left for making another attempted attack by the LW fighters. The P-38s had to stay with the bombers so forcing the LW to dive away saved the bombers.

Offline GScholz

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« Reply #44 on: May 04, 2004, 10:51:15 AM »
Quote
The cockpit heating problem was taken care of on the P-38L, the definitive
Lightning, which made up about half the production run.  But that didn't
help pilots in the ETO or MTO in 1943 and early 1944.  There were many
cases of pilots being forced to abort mission because their hands and feet
were frostbitten.

One problem the P-38 had in dealing with the Me-109, but not the FW-190
(which was more of a low and mid-altitude fighter) was the Me's high
altitude performace superiority.  Above 25,000 ft., cooling or
supercharger impeller or turbine speeds became limiting for the Lockheed,
and high speed capability started to fall off.  At low altitudes, the
plane could max out at about 330-340 mph.  This rose to well above 400 mph
between 25,000 to 30,000.  As the plane approached 30,000 ft, speeds over
Mach 0.60 could be sustained in level flight.  Thus, manuevering could
quickly give the plane compressibility problems.  At Mach 0.65 (290 mph
IAS, 440 mph TAS at 30,000 ft.; 360 mph IAS, 460 mph TAS at 20,000 ft.)
drag began to soar as the plane began to encounter compressibility.  At
Mach 0.67 shock waves began forming and buffeting began at Mach 0.675.  At
Mach 0.74 tuck under began. Buffeting developed at a lower Mach number in
any maneuver exceeding 1 g.
What this meant to a pilot in combat in say, a P-38H such as that used by
the 55FG or 20FG circa Jan. '44, was that if, at high altitude such as
Me-109s preferred approaching bomber formations, he locked on to the e/a
and it split-S'ed and dove away (typical Luftwaffe evasive maneuver), if
he attempted to follow, his P-38 would start to vibrate, then start
bucking like a rodeo bronco, the control column would begin flail back and
forth so forcefully it would probably be ripped out of his hands and begin
pounding him to crap.  Once the plane dropped down to lower altitude where
the speed of sound was higher, the buffeting declined and the trim tab
could be used to haul the airplane out of what seemed to be a death dive.
Recovery with trim tab resulted in 5 g pull-out.  Many a low-time service
pilot would be so shaken by this experience that he would never dive the
P-38 again, and might be so afraid of the airplane that his usefullness as
a fighter pilot was over.
The late J and L models solved this problem with the installation of a
dive flap.  Extend the flaps at the beginning of a dive and all problems
were eliminated.  Again, these models weren't available in the critical
period between fall 1943 and spring 1944 when the most desperate battles
against the Luftwaffe took place, and when the P-38s rep in Europe was
established.
The reason P-38s were as successful as they were in Europe (and it should
be kept in mind they performed their escort role before it was decided to
free the fighters from the bombers to seek out e/a on favorable terms so
they were always forced to engage on unfavorable terms) was at least in
part because they were wonderful aerobatic airplanes with absolutely no
maneuvers restricted except the dive.  Loops, Immelmans, slow and snap
rolls, Cuban eights...it could perform them all with perfection.  It had a
wonderful ability to perform in the vertical, with an excellent rate of
climb, splendid zoom climb.  It could easily change direction while
executing vertical maneuvers.  It was also a very stable gun platform,
being stable and very smooth while executing maneuvers.

In contrast, the P-51, had far fewer compressibility problems at speeds
normally encountered in combat, including dives from high altitude.  The D
model was placarded at 300 mph IAS (539 mph TAS, Mach 0.81) at 35,000 ft.
In a dive, the P-51 was such an aerodynamically clean design that it could
quickly enter compressibility if the dive was continued (in reality, a
pilot could, as a rule, catch any German plane before compressibility
became a problem).  But, say, in an evasive dive to escape, as the P-51's
speed in the dive increased, it started skidding beyond what the pilot
could control (this could be a problem in a dive onto a much lower-flying
plane or ground target--couldn't keep the plane tracking on the target if
speed was too high).  As compressibility was entered, it would start
rolling and pitching and the whole plane would begin to vibrate.  This
began about Mach 0.72.  The pilot could maintain control to above Mach
0.80 (stateside tests said 0.83 (605 mph) was max safe speed--but
structural damage to the aircraft would result).
The P-51's quirk that could catch the uprepared service pilot by surprise
was that as airspeed built up over 450 mph, the plane would start to get
very nose heavy.  It needed to be trimmed tail heavy before the dive if
speeds over 400 mph were anticipated.  However, in high speed dives, the
plane's skidding changed to unintended snap rolls so violent that the
pilot's head was slammed against the canopy.  Depending on how much fuel
was in the fuselage tank, on pull-out stick force reversal could occur, a
real thrill that could totally flummox a low-time service pilot diving
earthward at close to 1,000 ft per second trying to escape a pursuer.
The P-51 was a good dogfighter, positively stable under all flight
routines.  A pilot didn't have to work hard to get it to the limits of its
flight envelope (that is, he wasn't sweating heaving and pushing and
pulling and kicking to get it to move its ass.)  It was important to burn
down fuel in the fuselage tank to avoid longitudenal instabillity.
Cranking into a tight turn with too much go-juice in the tank would mean
instant stick force reversal and the pilot had to brace himself to oppose
the stick slamming backward into his solar plexus, and shove hard to
prevent the turn from tightening till, if he was lucky, he entered a high
speed stall, or, if unlucky, the wing ripped off.
Turns above 250 mph IAS were the killers, because they resulted in g
forces high enough to black out the pilot so that he couldn't oppose the
stick reversal and the Mustang would, unattended, wind itself up into a
wing-buster.


None of these vices are modelled in AH, and there are hardly a plane without such "quirks". At least some 109's had a problem with aileron overbalance at high speed; at least some 190's suffered from aileron reversal in tight left-hand turns; at least some Spitfires suffered from aileron reversal at high speeds etc. etc. etc.

AH is "easy mode" compared to real life, and no one should expect these simulated airplanes to behave exactly like the real thing. Airlines and the military pay millions for advanced simulators, and even they don't always get everything right. There are simply too many variables in real life to expect a lowly desktop PC to accurately simulate everything.
"With the first link, the chain is forged. The first speech censored, the first thought forbidden, the first freedom denied, chains us all irrevocably."