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So yet there is another reason why some people should not get "too" hung up on designer stats on planes. The ground crews very often modified their pilot's planes, in one way or another that affected it's flight characteristics.
Facts, Soren - toujours facts - where are your facts on any 109 out turning a 51 at high speed? and 'magnitudes better up to 300mph'?
I can do that math - the plural says at least 100 times better, singular says only 10 times faster.. ??
would you say that your powers of exageration are unsurpassed?
Show us the turn circle or time graphs at low medium and high altitude for low medium and high speeds in any flight test document you care to cite - US or Brit or German and you would have some credibility on this subject..
And last, but not least - It (the 109, the aces plane) was so 'unbeatable that it only lost some 10-20,000 fights? What is your definition of 'beatable'??
Hunter - I'm not at all sure of that - at least in the context of USAAF. Cass Hough and Pappy Gunn are two legends - who actually went through channels to a degree to make the Mods in a Service Group or in concert with say RAF for field modifications...
The 'heavy' nose for B-25's, the cheek guns for the B-25/26 in the pacific, the forward firing .50 cal guns in nose of B-17E and F' before the G incorporated the chin turret are examples of that. The exotic grafting of the B-24 Nose (with turret) on a B-17 is another example..plus Malcom Hood inst'l were performed (80+hour) at Service Group level
I have never seen or heard of examples of external (structural) changes made at the 'Line Chief' level.. On the other hand field installations of K-14 gunsights to retrofit to 51's to replace N-3/7's as well changes made to feed belts to reduce stoppages in both .50 cal (51D/K) and 20mm occurred at that level, found to be good and ECO's were propagated across Combat Groups while the changes/recommendations were passed back to Wright Pat and the MFR.
You might have some examples that contradict this during WWII?
Regards,
Bill
You used two examples I had thought of regarding US machines, but I have more knowledge of German planes and their history.
Don't get me wrong I am not saying every Tom Dick and Harry mod his plane.....I am just saying it was not rare to seen it done.
Guns added, removed (more then one P-47 pilot did that), guns upgraded, guns down graded, armor added, armor removed, different paint schemes (which affect speed greatly), waxing (added speed), cigar holders added (not that changed flight char. but it was funny), radios removed, ammo loads changed, etc etc. Many were done and done through unofficial levels. Every example I listed I have read about and I am sure I have missed some.
I am sure others (and you) could add more. How many planes out of say 100 were modified......I am not sure. But there was some that is forsure.
Does power-loading lift-loading ring a bell Bill ???
Oh, absolutely Soren, Does aerodynamics, combined with stick forces ring a bell with you?
Mustang Tacical Trials
BRIEF COMPARISON WITH Me.109G
Maximum Speed
45. The Mustang III is faster at all heights. Its best heights, by comparison, are below 16,000ft (30mph faster approx) and above 25,000ft (30mph increasing to 50mph at 30,000ft).
Maximum climb
46. This is rather similar. The Mustang is very slightly better above 25,000ft but worse below 20,000ft.
Zoom Climb
47. Unfortunately the Me. 109G appears to have a very good high-speed climb, making the aircraft very similar in a zoom climb.
Dive
48. On the other hand in defense the Mustang can still increase the range in a prolonged dive.
Turning Circle
49. The Mustang III is greatly superior.
Rate of Roll
50. Not much to choose. In defense (in a tight spot) a rapid change of direction will throw the Me.109G's sight off. This is because the 109G's maximum roll is embarrassing (slots keep opening)
Conclusions
51. In attack, the Mustang can always catch the Me.109G, except in any sort of climb (unless there is a high overtaking speed). In defense, a steep turn should be the first maneuver, followed if necessary, by a dive (below 20,000ft). A high-speed climb will unfortunately not increase the range. If above 25,000ft. keep above by climbing or all out level.
, can you ?? Show me please!
BRIEF COMPARISON WITH FW. 190 (BMW.801D)
Maximum speed
39. The FW.190 is nearly 50mph slower at all heights, increasing to 70mph above 28,000ft. It is anticipated that the new FW.190 (DB.603) might be slightly faster below 27,000ft but slower above that height.
Climb
40. There appears to be little to choose in the maximum rate of climb. It is anticipated that the Mustang III will have a better maximum climb than the new FW.190 (DB.603). The Mustang is considerably faster at all heights in a zoom climb.
Dive
41. The Mustang can always out-dive the FW.190.
Turning circle
42. Again there is not much to choose. The Mustang is slightly better. When evading an enemy aircraft with a steep turn, a pilot will always out-turn the attacking aircraft initially because of the difference in speeds. It is therefore still a worthwhile maneuver with the Mustang III when attacked.
Rate of Roll
43. Not even a Mustang III approaches the FW.190.
Looking forward to this !
LoL, ofcourse you want us to believe the graph done by the RAE AFDU ! You want to ignore the fact that the British test-pilots got scared shitless everytime the slats deployed and aborted the maneuver entirely. And if you don't believe me then go read the docs, there's plenty of mentioning of this.
Facts Soren?, Facts and data are a problem for you..
http://www.wwiiaircraftperformance.org/wade-turning.jpg
All you have to do of course is find a referencable expert source to negate this and representative trial data to refute this... which for 60 days you have avoided - because it dowsn't exist!
No wonder Mike Williams presents your posts on his site
i'm sure you are correct about all the examples you cited and more.. I'm also aware of co-axial cable and mast change, etc - but the structural stuff I'm pretty sure of also
Drgondog and Soren,
Guys keep it polite, debate sure but no name calling needed or insulting someone's homeland.
Why do present the AFDU tactical trials of the Mustang Bf-109G ?? Like I said the British test-pilots hardly even dared fly the 109! As soon as the slats came out they would aborted what'ever maneuver they were trying to perform emmidiately, convinced the a/c was about to stall
The slots open at about 110 m.p.h., and as they open the ailerons snatch slightly, and there is then slight aileron vibration. At 83 m.p.h. the aircraft becomes unsteady laterally and aileron buffeting sets in which increases in intensity as' the stall is approached. There is thus ample warning of the approach of the stall.
The aircratt stalled if the turn was tightened to give more than 4 g at speeds below about 200 m.p.h. The slots opened at about 0.5 g before the stall, and whilst opening caused the ailerons to snatch; this upset the pilot's sighting immediately and caused him to lose ground. When the slots were fully open the aircraft could be turned quite steadily until very near the stall. If the stick was then pulled back a little more the aircraft suddenly shuddered, and either tended to come out of the turn or dropped its wing further, oscillating meanwhile in pitch and roll and rapidly losing height; the aircraft immediately unstalled if the stick was eased forward. Even in a very tight turn the stall was quite gentle, with no tendency for the aircraft to suddenly flick over on to its back and spin. The Spitfires and Hurricanes could follow the Me. 109 round during the stalled turns without themselves showing any signs of stalling.
I was particularly interested in the operation of the slats, the action of which gave rise to aileron snatching in any high-g manoeuvres such as loops or tight turns, so I did a series of stalls to check their functioning more accurately. The stall with the aircraft clean, with half fuel load and the engine throttled right back occurred at 105 mph (168 km/h). This was preceded by elevator buffet and opening of the slats about 20 mph (30 km/h) above the stall, these being accompanied by the unpleasant aileron snatching as the slats opened unevenly. The stall itself was fairly gentle with the nose dropping and the port wing simultaneously dropping about 10 degrees.
I know you responded to Bill, but I had to comment on this...Back from holiday.
Bill,
Why do present the AFDU tactical trials of the Mustang Bf-109G ?? Like I said the British test-pilots hardly even dared fly the 109! As soon as the slats came out they would aborted what'ever maneuver they were trying to perform emmidiately, convinced the a/c was about to stall - fact is the 109 wasn't even approaching a stall !
Show us proof of that Soren - "Flight testing 101" - one of the first thing you ascertain is stall characteristics, that is needed to understand how the aircraft is going to behave at low speeds and landing. No properly trained pilot "should be afraid" of stalling an aircraft - that's just plain hogwash!!!The British test-pilots didn't push the Bf-109 past the deployment of the slats being afraid the a/c was about to stall, just like the new LW pilots. And the fact that the AFDU says the following only underlines this fact: "the Me.109G being embarrassed by its slots opening near the stall"
I didn't say they were afraid of stalling the a/c FLYBOYJ, I said they were afraid the a/c was about to stall when the slats came out in turns. The slats go *bang!* when they deploy in turns as the critical AoA is approached quickly, thus the slats deploy quickly, and this scared new pilots who weren't used to or knew anything about the slats. Stalling the a/c in slow straight flight wasn't a problem as the deployment of the slats was then slow and gradual, so no loud bang or notch was felt.
The proof is right infront of you.
Here Soren...
Jeffrey Quill, Chief Test Pilot for Supermarine, compared the Me 109E to
the Spitfire I as follows:
My experience in fighting against the BF. 109 E in a Spitfire Mk. I was
mostly around or above 20,000 feet and led me to the conclusion that the
Spitfire was slightly superior both in speed and rate of climb, that is
was a more 'slippery' or lower drag aeroplane, and that it was
outstandingly better in turning circle. 106
In October 1940 I flew a captured Me 109E; to my surprise and relief I
found the aileron control of the German fighter every bit as bad - if
not worse - at high speed as that of the Spitfire I and II with
fabric-covered ailerons. They were good at low and medium speed, but at
400 mph and above they were almost immovable. I thought the Me 109E
performed well, particularly on the climb at altitude, and it had good
stalling characteristics under g except that the leading-edge slats kept
snapping in and out. But it had no rudder trimmer - which gave it a
heavy footload at high speed - while the cockpit, the canopy and the
rearward vision were much worse than in the Spitfire. Had I flown the Me 109 earlier I would have treated the aeroplane with less respect in
combat.
Spitfire Mk I versus Me 109 E