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| Aviation Discussion on the aircraft of WWII. |
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| | #121 |
| Banned Join Date: Feb 2005
Posts: 6,625
| You didn't need to hands to fly it, come on, don't twist what I say now. You can also easily bank at high stick pressures by using two hands, but it's gonna take more effort than usual compared to an a/c with light stick forces. The a/c with lighter aileron forces will be able to enter different turns quicker and therfore shake off the attacker easier. Hence why the Fw-190 was such a deadly a/c, it was bloody hard shaking one off your six. |
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| | #122 | |
| IP/Mech THE GREAT GAZOO ![]() Join Date: Apr 2005 Location: Colorado, USA
Posts: 16,881
| Quote:
__________________ > I Support Doug Gillis < | |
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| | #123 |
| Banned Join Date: Feb 2005
Posts: 6,625
| I agree, accurate and precise manuevers are not to be made, but then again we're not talking formation flying here either The std. evasive maneuver in the Bf-109 was also pretty simple: A hard climbing turn. The roll into the banking position is where the 109 is slow, and thus it was about pulling back hard whilst adding as much aileron forces as possible, executing a form of half barrel roll. |
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| | #124 | |
| IP/Mech THE GREAT GAZOO ![]() Join Date: Apr 2005 Location: Colorado, USA
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| Quote:
__________________ > I Support Doug Gillis < | |
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| | #125 |
| Banned Join Date: Feb 2005
Posts: 6,625
| Well if we're comparing the a/c then why are you mentioning pilots ? Shall we compare them fairly or not ? As for the roll rate; If the timer was started at level flight, meaning the roll in was necessary, then this would have a bad effect on the 109's time because of the poor roll rate at speed. The Bf-109 first shined once it was in banking position and the stick was pulled back. Hence why the std. evasive maneuver was a sharp pull up into a climbing turn. |
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| | #126 |
| IP/Mech THE GREAT GAZOO ![]() Join Date: Apr 2005 Location: Colorado, USA
Posts: 16,881
| Its simple Soren, the 109 had a characteristic that placed it at a disadvantage as indicated herein. The situation is amplified with a novice flying the aircraft for obvious reasons. This goes back to my first point and this is if you're "double fisting" the stick at high speeds and your opponent is not, well, enough said.
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| | #127 |
| Senior Member Join Date: Jan 2008 Location: British Columbia, Canada
Posts: 524
| Here's some info that backs up the Soviet turn time tests on the Spitfire. The following clip is from R&M2381, June 1940. Note the turn time, 18.5 seconds (at normal power). Also note Clmax of 1.75.
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| | #128 |
| Banned Join Date: Feb 2005
Posts: 6,625
| Claidemore, That document shows the Clmax with the engine at full power, thus it's not the real Clmax. The thrust of the engine accelerates the the air over the inner parts of the wing, making the wing produce more lift in this region than compared to freeflow. The figure was calculated from indicated stall speed at full throttle which is lower than when gliding. At full throttle many WW2 fighters could hang in the air at surprisingly low speeds. Last edited by Soren; 06-28-2009 at 09:57 PM. |
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| | #129 |
| Senior Member Join Date: Jan 2008 Location: British Columbia, Canada
Posts: 524
| It's the Clmax of the plane in a combat turn, which I believe is what we are talking about. The Clmax of the 109 would be higher under the same conditions, perhaps 1.85 or 1.9?
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| | #130 |
| Banned Join Date: Feb 2005
Posts: 6,625
| Considering the freeflow Clmax of the 109 was 1.70 and the Spitfire's was 1.36, then I'd say around 2.00 to 2.10 at full throttle for the 109. |
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| | #131 |
| Senior Member Join Date: Jan 2008 Location: British Columbia, Canada
Posts: 524
| The Clmax figure of 1.7 for the Spitfire was achieved with the 960hp Merlin, not the 1050hp one in use by the time hostilities started. At that horsepower, clmax would be 1.85 for the Spitfire. RAE charts from R&M2361 show the 1200 hp 109E at 1.95 under power in a turn. So your assumed value of 2.0 for clmax of the 109F4 is probably pretty close. Interestingly, as G forces increase, the difference between clmax of the two planes decreases, at 5G it is 1.45 for the 109 and 1.42 for the Spitfire. I believe this is because of the elliptical wing of the Spitfire. That chart shows just under 20 seconds at 3G for the 109 (complete agreement with german specs) and just under 18 for the Spitfire Mk1. Lines up with the Soviet test pretty good too. In any case, when comparing P40E to 109F4, the difference in turn time is no more than 1 second. This is where pilot skill comes into play. In the low speed turning fight, the pilot who can keep the turn closest to the stall will win. The real advantage of the P40 is in the breaking turn at high speed. It's superior roll rate gives it a very good chance of getting into the turn quicker than the 109. The figures of max G computed for the two planes (7.44 and 6.43) don't have much relevance in real life. Both figures are above the blackout level.
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| | #132 |
| Banned Join Date: Feb 2005
Posts: 6,625
| Claidemore, Considering that the 109s Clmax was higher than the Spitfire's by a factor of 0.34 at freeflow I believe it will stay at this. So if the Spitfire at full throttle reached a Clmax of 1.85 then the Bf-109 would reach one at around 2.15 to 2.20. In terms of turn performance once in the banking position there's no doubt what'so'ever that the Bf-109 would outturn the P-40 at any speed, while being close to Spitfire which was only marginally better. Also remember that the British Clmax figures are calculations based on the turn performance achieved in British tests, and we all know that these are highly unreliable as the pilots were vary about going beyond slat deployment. Hence why a 190 Jabo did much better in their tests. As for the Soviet tests, they are interesting, but they aren't any form of proof. Measuring turn performance is a tricky deal, esp. if the timer is started in level flight. Last edited by Soren; 06-29-2009 at 01:21 AM. |
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| | #133 | ||
| Senior Member Join Date: Jun 2009
Posts: 153
| [QUOTE] Quote:
Quote:
VG-33 Last edited by VG-33; 06-29-2009 at 05:16 AM. | ||
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| | #134 |
| Senior Member Join Date: Jun 2009
Posts: 153
| Not at all, with a good triming you have no stick forces on a sustainted turn. You have just to mantain constant your speed, your banking angle, your AoA. The real problems will occur when you would need to change speed on altitude. Moreover soviet test are denouncing a lack of command effisciency and command respunse at high AoA on all the 3 axis. Probably because of the very small messerschmitt control aeras. Last edited by VG-33; 06-29-2009 at 05:14 AM. |
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| | #135 |
| Banned Join Date: Feb 2005
Posts: 6,625
| Bollocks on all accounts VG-33. A word of advice for you: Learn flight mechanics yourself before you start preaching about it to others! A max performance turn is made at or very close to the Clmax, pure and simple. You've openly denied this, clearly demonstrating your lack of knowledge on the subject. Keep digging VG-33. |
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