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Soren - I don't claim to know why the German engineers didn't provide boosted controls for the 109 but I am reminded that Lockheed did exactly that for the elevators on the P-38 to 'solve' compressibility dive recovery issue'.
Boosted elevators worked in the sense that control forces were manageably 'light' - but the airframe somehow lost it's tail in the process. I suspect without proof that neither the 109 aft structure or perhaps the wing structure were designed for high speed asymmetric load conditions that boosted controls would exacerbate.
I do know that Mustang designers provided REVERSE boost to rudder to INCREASE rudder pedal force requirements in dive and slow rolls - as the Mustang controls were too light, relatively speaking for those manuevers - and resulted in overstressing the airframe in certain assymetric load conditions.
the "1.8X" factor was a figure you regurgitated with no knowledge of the practices of German engineers, or, it is obvious that airframe structures engineering is not your core knowledge base but you wished to sound knowlegable??
I would have like to continued on this interesting topic, but , OK, whatever..
I am under the impression the Me-109 was designed for the DB600/601/605 engine. However early model aircraft had to make do with whatever engines were available while the new DB engine factory was being constructed at Genshagen.That the 109 could take the DB 601 engine was fortunate and good planning
I am under the impression the Me-109 was designed for the DB600/601/605 engine. However early model aircraft had to make do with whatever engines were available while the new DB engine factory was being constructed at Genshagen.
The Me-109 was at it's best during 1939 to 1940 when almost all the Luftwaffe pilots were rookies.
Imagaine a Hurricane or Spitfire designed around a Kestrel instead of the Merlin.
Even later models of the DB 605 can't help the "utiltiy" much. While they do improve straight line speed, climb and perhaps sustained turn (as opposed to a turn that bleeds off speed) they can't do anything for the higher wing loading and detoriating handling.
Many allied fighter planes on the other hand could (even if it wasn't smart) change roles from day to day. While many of the "modifications" to the 109 were supposed to be "field kits" I rather doubt that a squadron did bomber intercepts on Monday, bombing missions on Wednesday, and performed the anti-fighter role on Friday. While the 109 'type' fighter could perform all of these roles the individual fighters could not.
The small size also ment that the 109 never advanced in the ground attack/fighter bomber role either. While the 1100hp versions could carry a 250kg bomb the 2000hp versions couldn't carry anything bigger. And give the 605's appetite for fuel the likeily hood of getting very far with bomb wasn't very good.
The 109 by wars end had devolved back to a day fighter or short ranged interceptor and a rather tricky one for a low time pilot to fly at that.
Galland was a soldier and had a limited view. The main advantage the Bf 109 had over the Fw 190 was that it was much easier/faster to produce* while it performed as good as the Fw 190. Sure, the Fw 190 had advantages, and Galland was one of those who preferred the FW but then again, there were several pilots who preferred the Bf.Don't know if its true, but didn't Galland himself want Germany to drop production of the -109 in favor of the -190?
Actually, they were, they just evolved on paper before the Kestrel versions were put into production.
I guess you can say that to all late war aircraft - they were all greatly increased in weight, and thus wing loading, since wing area remained the same. Stall speed and turning circle as a result increases with wing loading, but as noted this is pretty much true for all major fighter designs of WW2.
No they were not. The Spitfire and Hurricane were both designed around the Merlin, their predecessors, the Type 224/ early type 300 and Fury Monoplane were designed around the Goshawk. The Kestrel was never considered for either type.
From sources I have read the Bf 109 always had a higher wing loading relative to its rivals and this meant that it suffered a greater degradation in its handling as a consequence of the ever increasingh power installed.
Also, measures were taken on later marks of Spitfire to address the deterioration in handling (such as the new wing on the mk 20 series. I am unaware if any steps were taken to address this with the 109?