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And you're still wrong.
Michael is completely right that the control surface volume is the design parameter for a the control surface (apart the airfoil of course). Yaw stability and responsivity both depend on the rudder volume, but yaw stability is achieved with less rudder volume than reponsitivity - so the latter is basically a design tradeoff between responsitivity and drag. Now if you don't believe that, get a textbook. -- Bert Willing ASW20 "TW" "Roy Bourgeois" a écrit dans le message de ... I think that the difference is that my original post focused on "rudder response" and others are focusing on "yaw stability" - which are different and somewhat opposite. The 1-34 is quite stabile in yaw but as Doug noted in his first post, it's response (time to desired effect) to your stepping on the pedal is pretty bad. I flew several 1-34s about 250 hours (and still occasionally). It doesn't have a problem with adverse yaw in a turn. But when you step on the pedal (say, to begin a slip) - nothing much happens (compared to other gliders). I was suggesting to Doug (and still believe) that the lack of rudder "response" is a function of the extraordinary fuselage length and that he would need a much bigger rudder to solve that problem. Now - if somebody will show me how to make my Nimbus 3 do ANYTHING responsively - I'll be eternally grateful Roy |
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