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#1
February 26th 05, 04:35 AM
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static thrust in pounds produced by tail rotor????????
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 
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