Vance and Emily Jaqua wrote:
Paul -read your twin fan concept with interest.
Thought you might like this curve of maximum thrust
from 500 hp for various flow "disk" diameters at
speeeds . This is no loss conversion into jet stream
power (perfect "pump") real expectations about
75 % of this at low speed to 90's above 250 or so.
3 eff sq ft drag area should be possible with clean
structure and good retracts - Vance
Thanks for sending that chart Vance. It looks very reasonably
to me. Would you be able to calculate what we would get out
of a 36 inch diameter fan with an 18 inch diameter hub... fixed
pitch fan?
36 inch gives me about 700 MPH tip speed at 6500 RPM if my calc's
are right. Dia X RPM / 60 = FPS
MPH = FPS X 0.682
Perhaps with a better blade we could go up to 38 or 39 inches.
I will revise my twin fan simulation accordingly.
Paul Lamar
The Aircraft Rotary Engine Newsletter. Powered by Linux.
http://home.earthlink.net/~rotaryeng/ http://www.linux.org