I can't figure this out. What does the RPM setting on the planes in AH actually do? Does anyone use this feature? As best I can tell, maximum cruising speed is achieved when you run with maximum RPM. This is not the way it's supposed to work. Am I missing something? Please explain this to me.
On a real aircraft that has a constant speed (or variable blade pitch) prop, engine performance is controlled by the throttle (manifold pressure) and by adjusting the angle of the prop blade (RPM). To achieve maximum cruise speed you would of course run with more throttle and drop RPMs (i.e. increase blade pitch to get more "bite") to a certain setting (published by the aircraft manufacturer) to achieve maximum cruising speed. The plane I am familiar with is the Piper Malibu. The manufacturer's published max cruising speed is 220 KIAS @ 20,000 ft. This is achieved by setting throttle at 24 in-mg (max is 32) and 2100 RPM (max is 2500). [I'm sort of guessing at these numbers but they are close] Trying to reduce RPM below that crosses over into diminishing returns and throttling up more than that overstresses the engine.
I have tried to use the same logic while flying, say the P51D in AH. I make an attack run then extend out and level off at 12,000 ft. I check my airspeed and I'm doing 400 MPH let's say. I go full throttle, kick off WEP, and begin backing off on RPM searching for that optimal setting. It appears to me that I have to max RPM in order to get max speed. Is this correct? The RPM seems to behave like a throttle rather than a "gear shift".
I probably should have experimented more before posting but I'm hoping someone already has figured this out and can explain it to me.
Thanks for any thoughts