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Dave - as I noted to Jim, I know what the design philosopy was on both the D and the H as I posted to Jim.
Simply I believe the handbook reference is in error... but I do believe the two airframes are EQUIVALENT across the board as long as the load out of fuel and ammo are the same - simply because the H would be 400 pounds lighter across the load profile
The simple math would look like this..
at 8000 pounds at 12G, the B and D wing would be designed to fail with 96,000 pounds applied to each wing
at 8000 pounds at 11.5G the H wing would fail at 92,000 pounds
at 8400 pounds the D wing still fails at 96000 pounds - but the 'allowable G' at that weight is 96,000/8400 = 11.42 G Ultimate ------> same as the P-51H with same loadout but lower gross weight at 8000 pounds.
The difference in real life is negligible but I don't believe the P-51H was 10% 'stronger'.
Part of stripping the weight was better design (straight leading edge/no strake, smaller main gear, etc), and pasrt was resizing caps and stringers after several years of failure history to better balance the structural integrity... so they a.) took out some unneccesary redundancy and b.) lowered the design limit and design ultimate accordingly based on reduced weights.
Thanks for you excellent explaination!
It was pretty simplistic Dave.. the more esoteric discussion then leads to point by point comparisons along the spars, the skin shears,the torqu boxes, the wing/wing and wing/fuselage fasteners to look at the stresses on each component to make sure they are less than "Ultimate Stress (Failure)"
and the internal wing designs were different enough that one may not 'assume" same loading conditions and load paths.
I am appreciatative of complexitive stress analysis. As responsible for generating impacts to upgrades for the B-2, I learned quickly that structual analysis was always important for any penetration of the composite skin of the bomber, like antennas. Load stress was carried by this skin and once interrupted by a penetration, detailed design was required to reroute the stress around the penetration. Since Boeing built most of the fuselage and wing, any antenna intallation was expensive!
Even the best pilot of the world have just two eye´s, while the numerical advantage at that time was extreme.
In early 1944, when the Luftwaffe still had some units and more good pilots(at least the disadvantage wasnt that big), even the 109G6 was good enough to counter the P51´s.
What is your definition "good enough to counter" the P-51s? I agree the relative merits of equality between the two ships but the German air force lost not because of inferior aircraft but because they lost their initiative to engage and fight the fighters. The relative ratios in air to air combat was very high in favor of the Mustang even before numerical superiority was existant. Remember, before June 1944 there were only two Mustang Groups (six total) to cover each of three bomb divisions (1500+ bombers total/300-500 each along a 20-30 mile tarck (each)..for target and withdrawal escort deep into Germany.
I always see the Vmax datas and sometimes also the climb performence(ceilling), what imho get forgotten when it comes to compare the dofight performence is the handling in relation to the altitude.
All true
As higher the planes get, as slower is the "middle IAS"(we dont always fly Vmax). When a combat start in high alt, the planes are very fast down to stall speed.
So we need to look much more to the slowspeed handlig then in low to medium alt, and here the FW190 most probably win, cause its advanced roll ratio, while the P51 suffer by its smal stall edge.
On the other hand the P51 can climb higher and is faster up there.
probably zero difference in stall characteristics between the two aircraft
What i want to say is: If the enemys saw each other and if both enemys did know what they do and if it was a 1 vs 1, noone would have been able to shoot the other down until they did reach low level(appart from a lucky shot).
That probably accounts for 80-90% of successful encounters
I cant see any good reason why someone would call one of this planes better than the other and its for sure nonsens to say one plane was better, cause the other got slaughtered, even the Me262 got slaughtered at that time.
The datas show very similar results, with a speed and climb advantage for the P51 in high alt, but at same time it must have had handling problems. In low alt the 190D had more power(best climb i saw is 1350m/min , 22,5m/s, 4428ft/min with 300km/h speed), on the other hand the speeds(IAS) was often higher and here the P51 also had a good handling, though close to the ground the FW190D had 400-500HP more power. btw, the typical combat weight of a P51D in combat area(after dropping the tanks) was 9600lbs(4360kg), cause the rear fueselage tank ALWAYS got used 1st, cause the plane was terrible unstable with this full tank.
Another btw, the german planes didnt look that good in the east cause the russian planes or pilots was that bad, it was rather the tactical situation, cause the russian bombers got mainly raped as "flying artillery". As such their fighters field of operation was also mainly in low alt, where their bombers was. This brought them into a same bad tactical position like the german pilots in the west and the russian HQ absolutly undervalue(or didnt care for) the need for a good high alt fighter performence, although in 1940/41 they had the best high alt fighter in the world(Mig 3). The realy bad habit to organisate all skilled pilots in elite squads, also didnt help to mass of the pilots.
I think the early rather high losses of the US fighters(also P51), against older planes than the FW190D9, show how important the pilot skill was. Still the US escort fighters always had the tactical advantage, cause the LW HQ commanded the LW fighters to attack the bombers, no matter how and they did split their forces all over germany, instead to of big mass attacks like Galland wanted them. As result the numerical advantage of the US fighters in combat area was bigger than is had to be.
What constitutes 'rather high losses in your opinion? And to the contrary, the LW controllers were VERY skillful at concentrating large numbers of fighters on smaller escort numbers all the way through 1944.
The LW fought like Wavell and Auchinleck vs the DAK, when Galland had his "1000" fighters, they got wasted in Bodenplatte.
Would have been interesting to see, what would have happend, when 1000 german fighters would have attacked mainly the escort. Like its was, we have no good possibility to value the P51D vs the german 1944/45 planes.
No, but there was EXCELLENT opportunity to evaluate during the Novemberr 1943 through June 1944 for the P-51B/C
Maybe in the future we will see a combat between the new FW´s and a old P51?? I guess that would help.
Greetings,
Knegel
nothing would have changed for the LW in 44-45 if they had the P-51 and the US the Dora
The safe wing load factor for the Fw190-D was 6.20 for wing ( 6.50 for engine mounts) and somewhat more more for the fuselage, according to Hermann. So the ultimate load would be 1.8*6.2 =11.2g. About the same as the P-51D.
Jim's posts are quite painful to read, because of the spelling, paragraphs, etc. So I cannot comment further.
German terms are simply "safe" (Sicher) load and "breaking limit" (Bruchgrenz):
"Die hierin aufgeführten 'Beanspruchungszustände' heißen 'sichere', weil bei ihnen noch kein Bruch auftreten darf, vielmehr noch ein vorgeschriebener Abstand von der Bruchgrenze eingehalten werden muss. Dieser Abstand ist die 'Sicherheit'. Die im Allgemeinen verlangte Sicherheit ist 1,8, das heißt erst beim 1,8 fachen der vorgeschriebenen 'sicheren' Belastung darf ein Teil der Konstruktion brechen."
LuftArchiv.de - Das Archiv der Deutschen Luftwaffe
See also "Leichtbau", page 31:
Leichtbau: Band 2: Konstruktion - Google Books
The designed gross weight for load factor of 6.20 was 4250kg.
For the Ta-152H the load factors were +5 to -2.5 at a design weight of 4500kg. (Hermann, p. 67)
just to point this out to you, JG 302 never had a high protection unit of any kind they flew on their own till dissolvement and the incorporation into the new III./JG 301in September of 44.
JG 301 only from November 44 when they received new A-9's did two staffeln of each the I. and II. gruppe provide high cover for their other two staffeln of each gruppe and in some ways when flying together as a whole Geschwader protect the Schwere gruppe the III. JG 301 many times did not fly entire ops together as a complete Geschwader. and just to back up a bit I./JG 300 really entered as the high squadron for it's 109G III gruppe and the ehavy Sturmgruppe the II.
even by December 44 with the 6./JG 301 having the inclusion of the Dora to the A-9 ranks it still could not keep up with speed, altitude and agility of the P-51D/K US escorts. nothing changed as the whole of II./JG 301 completed the transfer out of the A-9 to the Dora except for 8th staffel could they again keep pace with the P-51's. It just did not happen no matter whom wants to think otherwise. To make matters even more interesting Reschke states several times in his German/English work that their Doras really gave the P-51's trouble is a total mis-nomer. The only thing the Dora did for JG 301's pilots was give it a slight edge in the altitude department and then later meeting with Soviet fighters at mid range where it excelled.
What is your definition "good enough to counter" the P-51s? I agree the relative merits of equality between the two ships but the German air force lost not because of inferior aircraft but because they lost their initiative to engage and fight the fighters. The relative ratios in air to air combat was very high in favor of the Mustang even before numerical superiority was existant. Remember, before June 1944 there were only two Mustang Groups (six total) to cover each of three bomb divisions (1500+ bombers total/300-500 each along a 20-30 mile tarck (each)..for target and withdrawal escort deep into Germany.
Afaik the FW190A could get recovered very easy, while the P51 was a hand full.probably zero difference in stall characteristics between the two aircraft
I did read that around 70% of all WWII kills was made without that the attacked one saw the attacker(or much to late to evade).That probably accounts for 80-90% of successful encounters
What constitutes 'rather high losses in your opinion? And to the contrary, the LW controllers were VERY skillful at concentrating large numbers of fighters on smaller escort numbers all the way through 1944.
Imho not realy, cause there wasnt many situations, when the P51´s made sweeps and where the german fighters made sweeps, like it was common over russia.No, but there was EXCELLENT opportunity to evaluate during the Novemberr 1943 through June 1944 for the P-51B/C
Glad to see you join the forum..
Regards,
Bill
My thoughts on the Mustang are that it was a very energy efficient aircraft with low drag characteristics. Its surprising to me to see that its power plant was only producing a mere 1695hp at the peak of the war, which tells me that much of its speed took some time build up and accumulate.
By comparison, the Dora pushes 2100 hp with boost and normally i would think of German designs as very efficient.
whats interesting, though, is that Germany, apart from being ahead or on par with most of their aircraft technology, was trailing the successes found with American propellor innovations. Much of even the late war German prop planes still retained the three bladed coned shape props from the beginning of the war. Of course they had made some improvements and from what it seems the shape offers lower drag at higher speeds.
American propellors had actually gone from paddle blades to maximize climb to a sort of hybrid with the needle blades to allow for the best acceleration and retaining most of the top speed. In this light, its quite possible the lower powered Merlin produced more thrust than the Jumo, but even the Mustang took a lot of time to build up its top speed.
I guess my point to readers is to not be decieved by horsepower because prop blades and other factors can actually determine how fast an aircraft actually ends up going. If the contrast in propellor type were not so different, then i would say more power generally translates to more acceleration, and a better top speed.
Bill
My thoughts on the Mustang are that it was a very energy efficient aircraft with low drag characteristics. Its surprising to me to see that its power plant was only producing a mere 1695hp at the peak of the war, which tells me that much of its speed took some time build up and accumulate.
By comparison, the Dora pushes 2100 hp with boost and normally i would think of German designs as very efficient.
whats interesting, though, is that Germany, apart from being ahead or on par with most of their aircraft technology, was trailing the successes found with American propellor innovations. Much of even the late war German prop planes still retained the three bladed coned shape props from the beginning of the war. Of course they had made some improvements and from what it seems the shape offers lower drag at higher speeds.
American propellors had actually gone from paddle blades to maximize climb to a sort of hybrid with the needle blades to allow for the best acceleration and retaining most of the top speed. In this light, its quite possible the lower powered Merlin produced more thrust than the Jumo, but even the Mustang took a lot of time to build up its top speed.
I guess my point to readers is to not be decieved by horsepower because prop blades and other factors can actually determine how fast an aircraft actually ends up going. If the contrast in propellor type were not so different, then i would say more power generally translates to more acceleration, and a better top speed.
Bill
Knegel the high Alt. staffel from JG 51 was incorporated as a 4 staffel into one of JG 302's gruppen. nothing to do with JG 301
JG 301 flying Bf 109G-6's was so separated and did not function as a whole Geschwader till it's transformation in September of 44 when it received the Fw 190