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- W2897315663 abstract "Through curve fitting, the so-called flutter-margin method can estimate a good flutter boundary, however, is not suitable for the binary wing with a control surface. This paper develops the flutter-margin method and proposes a new stability criterion based on the dynamic equation of the three-dof wing and the Routh’s stability theory. The analysis of the trend and error-resistant ability show that: the new criterion, behaving a steady decrease to zero as instability is approached, varies in a sensibly linear manner with the velocity squared and could obtain good estimates of the flutter speed from data at a low speed, thus overcoming the defects of the velocity-damping method effectively. In addition, the criterion is more dependent upon the frequencies than on the decay rates, and is presented to be a good linear trend even when there is a 50 % damping maximum allowable error and 5 % frequency error." @default.
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- W2897315663 date "2015-01-01" @default.
- W2897315663 modified "2023-09-24" @default.
- W2897315663 title "A flutter boundary prediction method for the three-dof wing" @default.
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