Shoe
Posts: 170
Joined: 9/28/2003 From: Ridgecrest,
CA, USA Status: offline
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quote:
ORIGINAL: da Rock Actually, it's caused by an imbalance between the yaw stability and the roll stability. And truth is, it's cured by fixing or overpowering what ever is weak about the design that is causing it. I'm not sure what you mean by roll stability. If you release a directionally stable airplane at an angle of sideslip, it will yaw to reduce the sideslip angle (or return to the trim sideslip angle if it's not zero). I think that's what you mean by yaw stability. If you put an airplane at an angle of bank with zero sideslip, there's nothing to make it roll back to the original bank angle (with zero sideslip, there is nothing to tell the airplane which direction to roll). If you allow sideslip, the aircraft might roll back toward wings level, but that's due to spiral stability, not "roll stability". I'm just trying to point out that the roll axis is fundamentally different from the pitch and yaw axes. If you apply a coordinated roll input, you will not get a second-order response like you will in pitch and yaw.
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