Postby WhiteEagle » Thu Jan 19, 2012 10:08 am
The greater the pitch on the prop, the more drag it enduce, somewhere there is a cut-off point where it is of no use altering the pitch to a coarser value. This is also applicable to altidude, meaning the closer you get to MSL, the finer the pitch may be, lesser drag on the prop and the more trust you can get with more prop speed, it also depends on the Hp the enjin produce, coarser pitch = more Hp needed. What is interesting is that the reason for reduction gearboxes is the following. Any propeller's speed at the wingtips may not exceed the speed of sound, even thow the last couple of centimetres of a prop produces no lift at all, only from the centre to more or less 4/5 to the tip, the lengt of the prop is thus limited so that the tip travel to just under the speed of sound. We all know what happened to Chuck attemting Mach 1, as soon as he reached this, everyting worked in reverse. Not that the prop would suddenly starts to revearse, but it creates its own problems, hence the reason why no aeroplane fitted with a prop will ever be able to reach the sound barrier. It's not the plane that limit it, but the propeller's tip speed. O ja, three blade does NOT give more thrust that a 2-blade prop, it just run's quieter.
Best oil? Not that much proven difference between mineral and synthetic on the lube side, but definitly less carb build-up on synthetic. I only use Castrol products. Just my pennies worth.
"Good judgement usually comes from experience. Experience usually comes from bad judgement."