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« on: September 14, 2007, 12:01:12 AM »
In the CPs there is a discussion by either Burt, Dick, or Mike Mellville on running at "high" rpm---like 2700 to 2900 rpm. I encourage you to read through that----you can get the text online. In your "tin can" airplane, you are swinging a much heavier mass (aluminum propeller). Additionally, some engine/aluminum propeller combinations have a resonant frequency (certain rpm to avoid) that is destructive.
As I said before, full throttle (non turbo/non supercharger/non altitude compensating engine) is approx 75% at 8000 ft---and drops off from there. Ideally when you are trying to match your fixed pitch prop to your aircraft, here is what you are trying to do (and of course each one of these things is fighting with you---so you have to compromize):
--generate enough static rpm on the ground to be safe (can't remember what this number is----but probably around 2200 to 2300 rpm). If you can't generate the rpm, then you need a prop with less bite (assuming a properly running engine).
--generate the rpm you would like to cruise at---at your "normal" cruising altitude--at full throttle (assuming your normal cruise altitude is above 8000ft). If you have too much rpm up here---then you need more bite.
As you can see, if you need more bite at altitude, but can't generate the required rpm on deck, you are going to have to compromize---you may need longer runways with the bigger bite-----or accept a little more higher rpm at altitude.
I typically run between 2500 and 2700 rpm---depending on noise, how fast I am trying to get somewhere, how hot the engine is running, etc
An interesting note on LOP----engine has a different sound to it in this regime.