Hi Knegel,
>there must be a reason why they give the 109E in the manual absolut constant 15m/s up to 3500m, what seems to be very strange, specialy if we see that they reach 3500m in 3 min, what is pretty hopeless with 15m/s(900m/min).
Such diagrams were often simplified, perhaps in an attempt to make them easier to memorize for the pilots, perhaps to hide the unique engine technology (in the shape of the variable speed supercharger drive). The official Luftzeugmeister diagrams are most notable for this, but especially the climb rate below full throttle height is also simplified in British diagrams. Just like the Luftzeugmeister did in the Emil diagram, the RAF liked to draw climb rate below full throttle height as a constant figure though in reality, it wasn't.
There is more one should keep in mind about performance diagrams: For example, they were usually corrected to a constant weight (often, but not always, the take-off weight), and the time to altitude diagrams were (as far as I can tell) normally calculated from the climb rate diagrams by simple numerical integration. This leaves weight loss due to fuel burn as well as the requirement to add kinetic energy to the airframe unaccounted for, but for fighters, both effects are minor anyway. (The "climb rate" diagrams could more accurately be considered specific excess power diagrams as a result.)
Anyway, here is a calculation of the Me 109E performance I prepared a while back:
http://hometown.aol.de/WBHoHun/Me109E_DB601A-1_early.gifIt still features some simplifications, mainly the approximated power curve which leads to a somewhat angular graph between 1.5 km and 4 km. This should be a smooth curve realistically.
I'd say the climb rate in the diagram you posted is probably for 1.23 ata/2300 rpm, though it indicates a full throttle height that is too low for that. This is a bit odd, but considering the somewhat inaccurate nature of the simplified graph, nothing to worry about :-)
Regards,
Henning (HoHun)