Hi
I need a perspective so this is a general question . If a 6 foot dia.
tail rotor is turning 2500 rpm how many pounds of static thrust at a
particular pitch angle would be produced???? And is that for a flat
rotor blade meaning no helical twist. Any senario close to the above
would be a big help. I want to build a variable pitch rotor and need to
get an idea on the thrust output .
Thanks ED