Thank you ,Sir.


The OTHER Kevin in San Diego wrote:
On 25 Feb 2005 20:35:40 -0800, wrote:

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

A note to Frank Robinson would probably go a long way towards
determining the answer. He's regarded as quite an authority on tail
rotor design.. Don't know how you'd get in touch with him, but a
phone call might get the ball rolling.