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Me262 test pilot Hans Fay maintained that the Me262 had "poor maneuverability", though he also said it turned better at high speeds than at low. He also said it had good response to ailerons at all speeds. Obviously those comments are pretty open to interpretation!
The only account I have read of an Me262 engaging in a turn fight was against Ivan Khozedub, and that resulted in Khozedub shooting down the 262. There may be others, but I haven't read them.
I calculate a turn radius of 4930 ft and time of 46 seconds at 450 mph pulling about 3 G in a Me262. Sustained turn rate at this speed will be about 6.5 degrees per second according to the charts posted earlier. A Spit or Mustang, 350 mph, @ 3G, radius is 2980 feet and time of 36 seconds and could have a sustained turn rate of about 8 degrees per second at that speed. The prop fighter can definately outturn a jet fighter by not trying to match it's speed, and staying inside the jets turn. Note: it takes the prop fighter 1.5 to 2 seconds to relax it's turn and 'cut across the circle' to close to firing range in that scenario, albeit a fairly short firing time given the speed difference.
There is a proplem with claiming a dogfight advantage in a plane because it retains speed better in a turn. IF both planes try to stay at 400mph, the jet is going to have an advantage, but what prop pilot is going to try to keep his speed up while a jet is closing on his tail? It's just not going to happen in the real world, he's going to increase his turn, and because he can lose speed quicker (more drag), he will turn tighter, denying the jet a firing solution.
The jet has an enormous tactical advantage with its superior speed, and will use that to dictate an energy fight, rather than an 'angles' or turning fight.
As for climb, Soren posted a chart here:
http://www.ww2aircraft.net/forum/aviation/me-262-performance-12011.html
-which shows projected climb times for a 004C Jumo engine (more powerful than the 004B engines used in production 262s). It shows a climb time to 10 k at full weight of 19minutes, and 10 minutes at reduced weight. Real operational weight would be somewhere between those two figures, and climb rate of an operational 004B engined 262 would be a bit lower. For arguments sake, even if we use the data for the 004C, the climb rate is at best only at par with contemporary prop fighters and fully loaded, it's not as good.
However, the 262 would zoom climb better due to it's high speed, and to be fair, 'best climbing speed' was faster. In essence, it might not gain altitude on a pursuing Mustang or Spitfire, but would gain distance during the climb. (this is backed up by combat reports against 262's, they usually escaped in level flight or shallow dive) Either way, the prop fighter isn't going to catch it.
The Me262 was a very good fighter, with a kill ratio of 5-1 (maybe 3-1 if you correct for overclaiming). But lets put the credit for that success where it belongs, vastly superior speed and firepower, not dogfighting ability.
Davparlr,
A jet looses speed in maneuvers much much more slowly than a piston engined fighter, the reason being a Jet is a MUCH cleaner a/c, and at high speeds its also got more power available. This is simple fact, there's no point in trying to deny it Davparlr.
I don't think a propeller produces drag when it is producing thrust equal to or greater than the aircraft drag.And this is pretty much universal when comparing Jets to propeller a/c, as the prop whilst generating allot of thrust also generates allot of drag
At the same time the efficiency of the prop falls off quickly as speed increases, whilst the Jet keeps a constant amount of thrust during the entire speed regime.
The P-80 has a zero lift drag coefficient of .0134 and the P-51 has a zero lift drag coefficient of .0161, the P-80 has 83% of the drag of the Mustang, not a lot. An F-4 Phantom has a zero lift drag coefficient of .0224, or, not as slick as the P-51.So FLYBOYJ is completely right when he says that Jets are allot slicker than piston engined a/c.
And like he says Jets are very reluctant to loose speed, which is one of the prime reasons you need reschooling before going from piston engined a/c to Jets. This very high energy retention is one of the major suprises to the German test pilots when they first flew the Me-262, the reluctance to loose speed during the turn in approach often forcing them to go around for a second try. (I'm sure FLYBOYJ has had a couple of these as-well when he first started flying jets)
claidemore said:There is a proplem with claiming a dogfight advantage in a plane because it retains speed better in a turn. IF both planes try to stay at 400mph, the jet is going to have an advantage, but what prop pilot is going to try to keep his speed up while a jet is closing on his tail? It's just not going to happen in the real world, he's going to increase his turn, and because he can lose speed quicker (more drag), he will turn tighter, denying the jet a firing solution.
Soren said:As long as the speed was kept above 450 km/h the Me-262 has the advantage in acceleration, and therefore angles fighting.
Now since the average pilot couldn't withstand much more than 5 G's the Me-262 will have the advantage in an angles fight at speeds above 450 km/h. So unless the pilot in the piston engined fighter pulls over 5 to 5.5 G's at 450 km/h (or way above that as speed increases) he isn't going to get out of the Me-262's sights.
Now ofcourse if the turn fight is prolonged and the piston engind fighter keep decreasing its speed to below 450 km/h then the Me-262 will have to break off and regain energy.
I somewhat agree, as a very sharp and prolonged tight turn quickly can cut speed to down below 450 km/h. However if the engagement speed is 600 km/h the Jet can easily afford to pull lead for a while before having to break off and regain speed.
While you are correct you describe the "slickness" I spoke about. The jets I've flown seem like they don't want to slow down, but their engines are slow in spooling up, a somewhat tricky situation. In a propeller driven aircraft it accelerates quickly and slows down quickly.Again, when you pull the throttle back on a prop job, the propeller starts generating drag as the air flow tries to turn the propeller (in a piston engine, this is against engine compression). In a jet, when you throttle back, no drag is created. If you could feather the propeller, or if the propeller fell off, I think you would find it much harder to reduce speed as compared to an unfeathered prop and be more similar to a jet. This is the main force differentiating flying final in a prop or a jet, not the "slickness" of the airframe.
Davparlr,
With lift comes drag, it's inevitable. Thus while a prop certainly provides thrust, it also generates drag.
As to the Cd0 figures where did you get these from ? (I suspect the P-51's is for a mock up a/c without a prop)
The Cd0 of the Me-262 is 0.0115 IIRC.
As for the Phantom, well that's not surprising at all, Cd0 of many modern fighter s quite high, but their thrust figures are at the same token also extremely high.
Now since the average pilot couldn't withstand much more than 5 G's the Me-262 will have the advantage in an angles fight at speeds above 450 km/h. So unless the pilot in the piston engined fighter pulls over 5 to 5.5 G's at 450 km/h (or way above that as speed increases) he isn't going to get out of the Me-262's sights.
Now ofcourse if the turn fight is prolonged and the piston engind fighter keep decreasing its speed to below 450 km/h then the Me-262 will have to break off and regain energy.
I've only seen it in one place and it showed .02, but I have no confidence in the site, could be a gamer site.
Hehe, the Me-262's Cd0 is far lower than the P-51's that's for sure, and lower than the P-80's as-well.
.02 is waay too high and in the same league as the 109 Spit.
Where did you see the figure ?
As for propeller drag, well a prop works by generating lift, creating a low pressure infront of itself and a high pressure behind itself. With this lift however comes drag, but despite this there's also the frontal disc area of the propeller, the props themselves being hit directly by the airstream. Hence why no prop fighter is able to brake the sound barrier, the prop simply generates way too much drag at high speeds.
The Jet fighter on the other hand is very "slick", being much cleaner than the piston engined fighters, lacking all the cooling ducts etc etc. Hence why everyone who flew the Me-262 noted how it kept its speed in tight turns much better than any prop fighter, German, UK US pilots all noting the same.
Well one well known aerodynamic resource book, Hoerner Fluid Dynamic drag by S. F. Hoerner, gives the following values:
Table on page 14-9:
P51 Mustang: Cds=0.017
Me262: Cds=0.021
P-80: Cds=0.02
Cds is drag coefficient based on wing area which I assume you refer to as Cd0 above.
I gather you are convinced that the opposite is true (that Me262 has a lower Cd0 than the P51). What do you base this on? Source?
Hehe, the Me-262's Cd0 is far lower than the P-51's that's for sure, and lower than the P-80's as-well.
.02 is waay too high and in the same league as the 109 Spit.
Where did you see the figure ?
As for propeller drag, well a prop works by generating lift, creating a low pressure infront of itself and a high pressure behind itself. With this lift however comes drag, but despite this there's also the frontal disc area of the propeller, the props themselves being hit directly by the airstream. Hence why no prop fighter is able to brake the sound barrier, the prop simply generates way too much drag at high speeds.
The Jet fighter on the other hand is very "slick", being much cleaner than the piston engined fighters, lacking all the cooling ducts etc etc. Hence why everyone who flew the Me-262 noted how it kept its speed in tight turns much better than any prop fighter, German, UK US pilots all noting the same.
Just an aside but Cd0 is CD at zero lift to take induced drag out of the equation. I suspect the induced drag is also higher for both the P-80 and Me 262 but I haven't looked - so the statement is from a place where the sun does not shine.
Hehe, the Me-262's Cd0 is far lower than the P-51's that's for sure, and lower than the P-80's as-well.
.02 is waay too high and in the same league as the 109 Spit.
Where did you see the figure ?
Just an aside but Cd0 is CD at zero lift to take induced drag out of the equation. I suspect the induced drag is lower for both the P-80 and Me 262 but I haven't looked - so the statement is from a place where the sun does not shine.
Hehe, the Me-262's Cd0 is far lower than the P-51's that's for sure, and lower than the P-80's as-well.