I'm currently working on a video comparing the Spitfire Mk I and Bf 109 E-4 when it comes to turn performance, and which I will post on YouTube when it's finished.
By necessity, it will of course only cover parts of what you will find in my book. And you can read more about the subject there.
But in the meantime, here are a few slides from the video to give you an idea about what it will cover.
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Note that the British are missing something here: They thought they were extracting the Bf 109 E's best turn potential just at the point when the slats were opening in these trials.
So in summary, these trials are pretty much useless for comparing the Spitfire's and Bf 109's turn performance. And yet you will se these trials referenced in much litterature.
Now compare that to what Steinhoff is saying: Real manoevering only begins when the slats have come out fully, and which is also assumed as the limiting factor in the two slides below.
An interesting thing to note here, is that the Bf 109 E can actually out-turn the Spitfire Mk I at lower altitudes by dropping flaps, which I found somewhat unexpected.
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In fact, the Bf 109 could use any amount of flap the pilot chose for manoeuvre. 0.5 Degree, 3.25 degree, 20 degree, whatever, because it was infinitely variable on a screw thread.
So, automatic manoeuvre slats with flap was a Bf 109 speciality that is not defined.
Modern in flight assessment of Bf 109 Slat operation has shown that Slat operation was not a disturbance to flightpath, it just progressively increased the Cl Max and droop ailerons on the early models had a further slow speed improvements with flap.
The Bf 109 Pilot could also select the cooling flaps closed to reduce drag for short periods in a combat.
Finally, here the Bf 109 power setting to compare with the Merlin 12lb Boost would be 1.42 ata at higher rpm as well.
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