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This reveals that the torsional aerodynamic damping derivative A∗2 reaches a positive maximum followed by a continuous decreasing tendency and eventually negative A∗2 values are identified.
(ii) is eventually negative.
From, we have that is eventually negative.
(3) The inequality (3.3) has an eventually negative solution.
There are not eventually negative nonoscillatory solutions of (1.1).
Suppose that there exist eventually negative nonoscillatory solutions of (1.1).
The inequality (3.3) has an eventually negative solution.
(3) The inequality (3.3) has no eventually negative solution.
The case where (x t)) is eventually negative is symmetric.
Then it is either eventually positive or eventually negative.
Therefore, is either eventually positive or eventually negative.
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