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• W3174958356 abstract "The dynamics of a helicopter blade in forward flight are described by a system of linear differential equations with periodic coefficients. The stability of this periodic aeroelastic system is determined, using multivariable Floquet-Liapunov theory. The transition matrix at the end of the period is evaluated by: (1) direct numerical integration, and (2) a new, approximate method, which consists in approximating a periodic function by a series of step functions. The numerical accuracy and efficiency of the methods is compared, and the second method is shown to be superior by far. Results illustrating the effect of the periodic coefficients and various blade parameters are presented." @default.
• W3174958356 created "2021-07-05" @default.
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• W3174958356 date "1974-04-17" @default.
• W3174958356 modified "2023-09-25" @default.
• W3174958356 title "Aeroelastic stability of periodic systems with application to rotor blade flutter" @default.
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• W3174958356 doi "https://doi.org/10.2514/6.1974-417" @default.
• W3174958356 hasPublicationYear "1974" @default.
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