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- W2364659661 abstract "Employing regression analysis ,the simulation models of aggregate vibration acceleration and aggregate stresses with respect to aggregate sound pressure as well as the simulation models of aggregate stresses with respect to aggregate vibration acceleration of an aircraft flap under acoustic excitation were given. The limitation of the linear and non-linear relationships of the structural stress response and structural acceleration response to the aggregate sound pressure as well as that of the structural stress response to the aggregate acceleration response were obtained via pattern recognition." @default.
- W2364659661 created "2016-06-24" @default.
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- W2364659661 date "2004-01-01" @default.
- W2364659661 modified "2023-09-27" @default.
- W2364659661 title "Sonic fatigue stress simulation and pattern recognition of an aircraft flap" @default.
- W2364659661 hasPublicationYear "2004" @default.
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