by Tony » Fri Jul 27, 2007 6:38 pm
Mike, in theory, the flow geometry we are dealing with here could be thought of as being fairly similar to that of a poppet valve. For a constant flow area, valve "lift" needs to be one quarter of the incoming throat diameter.
A four inch entry pipe could flow into a rotor that was one inch wide at the entry point, and the flow "curtain area" would then equal the pipe flow area. That is the basis.
The other aspect is that the air in the rotor is accelerated, and it can do that more easily if the flow area tapers down smaller as the air moves outwards tangentially. That is a bit of a tall order for a home made rotor, but it can be approximated by flaring or dishing the hub area outwards between where the blades start, and the entry hole. Fortunately the blade area can have parallel walls, and the blades themselves need not be made very long.
We can get away with all this reasonably well because the pressure ratio is quite low.
Thinking about this a bit more, my approach to building a rotor cover would be to have a four inch entry hole, and that provides a flow area of 12.5 inches.
If my basic rotor design width was half an inch, the rotor flow area starts to fall to less than 12.5 square inches inside a pitch circle with a circumference of 25 inches, maybe eight inches pitch circle diameter. So the flare would be an inch wide at four inch diameter entry, and taper down to half an inch wide at eight inches diameter.
That would also place the half inch wide rotor about dead center in an inch and a half wide housing.
Also known as the infamous "Warpspeed" on some other Forums.