renrich
Chief Master Sergeant
There is the proof about the landing gear!
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From the people who built the 262 replicas
"As the landing gear was known to be another weak area on the original Me 262, a detailed analysis of landing gear stresses was directed. This process revealed that a shock loading was generated by the spin-up forces of the large, heavy main wheels, which had to be reacted into by the wing landing gear attachment structure. This placed a severe demand upon wing spar area and the airframe simply had to absorb these forces. Over time, this would have had a devastating effect upon the aircraft."
Me 262 PROJECT TECHNICAL DATA
I'm trying figure out just what issue they defined.
Joe - Virtually all wing mounted gear was/is designed to absorb both shock and bending in the main spar, so the 262 by that definition would not have been any different.
Larger wheels would tend to create more eccentric loads to a yoke (than smaller tires) before being resolved into compression and shear loads on the strut. The torque box design should be designed to transmit the torque created by lateral loads on tire into shear panels while the rest (vertical) Has to be taken by the Spar and translated to the fuselage structure designed to take all the wing loads..
Agree - it seems someone on the replica team saw something really wrong when analyzing the original design.
I think the biggest problem would be with a drawn seamless tubing for the landing gear of an aircraft that would have to operate off of grass strips, evidently the gear was built for mass production. I read on several occasions that this was a problem with the 262. Adding low grade steel trunnions and link fittings didn't help, but then again the need at the time was to have the aircraft rapidly produced.
FLYBOYJ I concede regarding the landing gear, just reread some of my books and there were indeed even a few Me262's which crashed on hard landings due to a landing gear failure. Doesn't say wether it was the main landing gear or the nose gear which failed though in any of the cases.
Very true - I've seen lead times as long as a year for certain types of aircraft.They sure as hell didn't have the luxury of doing forgings or castings with the 'lead times' available to them..
Was watching the latest rendition of "Dogfights" the other night and reflecting on fights between F4s and Mig 17s and comparing that to a fight between the ME262 and a P51. The F4 had a huge advantage in speed but could not stay with a Mig 17 in turn so had to adopt energy tactics to compete. Strikes me that the ME262 faced the same problem with the P51. Were the ME262 pilots able to utilise the same energy tactics as the F4s did?
All you needed was one airplane with a better performance advantage over the rest and it needn't be an extreme advantage. The pilots took it from there. Though the 262 was fast, it was too fast. It had hitting power but those weapons were slow muzzle velocity, in-close weapons that put the 262's performance disadvantageous to it's purpose as an interceptor. Yea, it could scoot but it couldn't scoot and be an effective weapon at those speeds. It needed to be flown slower to put the pilots in-close with sufficient time-on-target to bring their cannons in where they were most effective. Engine spool-up was slow so speed recovery was slow. At high speed there was little time to put enough fire power on any given target, not to mention the very real target fixation that got many pilots in trouble by staying too long on a firing run and wrenching the crap out of the plane to avoid hitting the target. At 500 MPH closing speed, there's precious little time from the instant a target is within effective range to the moment of collision and head-on attacks at those closing speeds of 7-800 mph were a pointless waste of ammunition. Tactics for using an extremely high-performance, easily flamed (fragile) airplane against a very slow moving target required reducing performance to stay with that target. In that performance envelop the 262 was outmoded by the P-51, hands down.
If an ME262 is Making a run on the P51 from the 6:00 position at 450 mph and the P51 is doing 350 mph and pulls a max G turn, can the ME262 turn inside the P51 in order to pull lead? A comparable example would be a Corsair at 350 mph and an A6M at 250 mph. Under those conditions the USN told their pilots not to dogfight with the A6M.
all of this applies to a "far fight" which the prevailing conditions in the war didn't allow for. so the Me262 had a great advantage in a fight that it wasn't in. It's like taking a semi-auto pistol into a room full of people carrying six shooters. Advantage? None that matters.Pulling lead on your opponent is not the same as going into a furball with him Renrich. If a Zero pulled a straight turn with a F4U on its tail it would present a very nice target for the incoming F4U. The F4U pilot just has to note the direction of the turn, pull lead and squeeze off a 1 second burst. Chances of a hit are good. And the exact same goes for a P-51 with an Me262 on its tail.
The best move for the Zero would be to do a half barrel roll and then reverse direction by pulling out. This will make targeting extremely difficult for the incoming F4U and force it to either try and follow the maneuver, which it cant cause it's going too fast and the Zero is at an advantage in an angles fight, or climb for another attack. And again, the exact same goes for a P-51 with a Me262 on its tail.
In the end though the nimbler but much slower opponent is at a serious disadvantage as the more powerful opponent will be able to completely dictate the whole engagement, going in for pass after pass until a successful hit is made. And neither the F4U or Me262 needed many hits to down their opponents in question.
See, I read it as "Which fighter brought the biggest new advantage to the war effort?" not "Which fighter brought the biggest new advantage to a hypothetical individual air duel?"Well I wasn't really talking about the advantage it gave the Luftwaffe as a whole Clay, only the advantage it gave the individual pilot. The Me262 was the a/c which introduced the greatest advantage any plane ever had over the rest. In the big picture it ofcourse wasn't enough however, seeing that it was usually outnumbered 12 to 1 by Allied escorts, but that's not what the thread is about as I see it.