Andy Walker wrote:I'm curious who voted "negative dynamic stability." If I'm remembering my aerodynamics correctly, that means that if you put the aircraft in an oscillation state (say, but 'flicking' the stick back and then releasing it), it will continue the oscillation (in this example, pitching first up, then down), in ever increasing amplitude, until actively corrected or until the airframe can no longer handle the forces acting on it.
This is the worst possible handling trait for an aircraft, and is very dangerous. I certainly have never seen this kind of behavior from a Sonex/Waiex/Xenos. I have always heard of the Sonex described as having neutral stability on all axes, and in fact recall John Monnett stating that is how the airplane is designed to behave.
Am I wrong or have my definitions confused?
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