Most WWII aircraft had constant-speed airscrews. I'm sure the pitch settings for various stages of flight would be marked on a plate on the panel or on the quadrant itself. All aircraft would use full power/fine pitch for take-off (presumably 100% in CFS2). This would then be reduced as soon as possible for climb to prevent overheating. It would be reduced further for optimum cruise & fuel economy. I'm not sure of the ideal setting for air to air combat.
The power is indicated on the tachometer (rev counter) & the boost gauge. Boost (on RAF aircraft) is measured in + or - pounds per square inch (often referred to as inches), for example: optimum climb for the Spitfire Mk I is 2,850 rpm at +12 lb/sq. in. boost. On the Spitfire Mk IX with the Merlin 66 + 2-stage supercharger, maximum boost is quoted at 3,000 rpm & +25 lb/sq. in. for combat climb and all-out level conditions.

I notice the CFS2 default panels use a manifold pressure gauge which works on a slightly different principle. It indicates the atmospheric pressure (actually suction) inside the intake manifold measured in inches of mercury (In/Hg).

Another thing I'm not sure about is if the M$ flight model takes supercharging into account.
As I've often said before, this is a highly complex subject & here's me pontificating on things I know far too little about. I will need a long lie down in a darkened room to recover from all this. LOL
All you really need to know is what I mentioned several replies ago. Use Fine pitch for full power (take-off & landing). Coarse pitch for nomal flight.

If you really want to know more, read this. http://www.avweb.com/news/columns/182081-1.html
I'm going back to my jets.
