Pyro- I already sent you a mail with a big attachement. I will sent you some other data now, one is a propeller test with a K and a 605D engine. It shows clearly the max speed at combat power (1,35ata, 2600 u/min)- top speed at 8500m (without mw50).
I have a copy of an original table of Daimler-Benz, dated spring 44.
It says:
DB605A
Fuel B4, propeller adjustment by hand
compression 7,3/7,5
full-pressure-height: 5700m
takeoff and emergency power:
ground: 1475HP @2800u/min, 1,42ata(pressure)
fph: 1355HP (5700m!)
10000m: 790HP
15000m: 320HP
DB605AS
Like 605A, bigger supercharger of the 603G
compression 7,3/7,5
full-pressure-height(fph): 7500m
takeoff and emergency power:
ground: 1435HP @2800u/min 1,42ata
fph: 1225HP (7500m!)
10000m: 890HP
15000m: no data
DB605D
Like 605A, bigger supercharger, propeller adjustment works automatic, fuel C3
compression 8,3/8,5
full-pressure-height(fph): 8500m
takeoff and emergency power:
ground: 1435HP @2800u/min 1,42ata
fph: 1210HP (8500m!)
10000m: 1000HP
15000m: 410HP
All data without mw50 or gm1
wells posting imo the clue to the solution, i think. I know thatin many books who find for top speed of a 109K an altitude of about 6000m, with much higher number of HP- Wells is right i think, there they used mw50, and therefore the critical altitude dropped- i dontīt know why but it seems to be a fact.
I have another data for the 605D, now with mw50:
takoff and emergency power:
ground: 2000HP @2800 u/min 1,98ata
5500m: 1800HP @2800 u/min 1,98ata
climb and combat power:
ground: 1800HP @ 2800 u/min 1,8ata
6000m : 1530HP @ 2800 u/min 1,8ata
It really looks like that with mw50 the critical altitude dropped.
BUT without mw50 (and i did my speed tests like wells did them without wep, and my climb tests too) the critical altitude should be much higher than it is now.
niklas