Hi Juha,
>the figures Vincenzo gave for FAF H75A are not figures Finns got from their own tests.
Ah, very important to know!
>Max for CUc (c=Cyclone) was appr 480km/h at FTH.
Was the full throttle height also given?
>According to British test in Apr 41 max for H75A-4 was 486km/h at 4300m, max climb at 2870kg 13,2m/s and ceiling 10 300m
Hm, I can't quite understand the 4300 m full throttle height, and how the aircraft could be so much more draggy than the official Curtiss numbers would indicate, but 13.2 m/s and 10300 m ceiling at this weight appear perfectly in line with the powers given for 2300 rpm.
>The propeller was 3 blade Curtiss Electric constant speed, diameter 3,07,m blade angle moved between 29-52 deg
Thanks! Another vital bit of information
>On 100oct, maybe German C3, LeR 1 had a small secret cache of it to be used in Curtiss for to hunt high speed Pe-2 recon planes, but 87 oct was the standard fuel of FAF
I see. No idea what the 87 octane power limits were on that engine if combat use was considered ... I'll have to see if the FM-2 manual has something to say on that.
Here is a comparison of my calculations for the Curtiss. #1 is for the 520 km/h @ 4.6 km data point, with some leaps to salvage some logic. #2 is for the 486 km/h @ 4.3 km data point, ignoring the higher full throttle height that appears inevitable even with a modest amount of ram effect - thus the top speed exceeding 486 km/h and being reached at almost 5 km.
#2 shows good agreement in the climb data with the British test results you provided if we consider it to be valid for 2300 rpm. At the full 2500 rpm that the R-1820-87 probably used for Military power, performance would be a bit better, as indicated by the thick line.
Regards,
Henning (HoHun)