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- W2169968014 abstract "The paper extents the classical nonlinear panel flutter problem to the analysis of the effects of harmonic excitations over the auto-oscillating structural system This phenomenon can be governed by the turbulent boundary layer, by the oscillating shock wave or by the acoustic noise. The present study is limited to the case of uniformly distributed pressures (with imposed law of oscillation in frequency and amplitude) acting on isotropic simply-supported square panels also subjected to aerodynamic and thermal buckling loads. Forced oscillations are compared with flutter motion on the same time-domain diagram (obtained by using timedelayed harmonic excitations) in order to observe the transition self-excited-* forced vibrations and to extract the necessary information for a reliable structural design." @default.
- W2169968014 created "2016-06-24" @default.
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- W2169968014 date "2000-09-06" @default.
- W2169968014 modified "2023-09-22" @default.
- W2169968014 title "Combined forced-self-excited oscillations of panels under aero-thermo-elastic conditions" @default.
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- W2169968014 doi "https://doi.org/10.2514/6.2000-4790" @default.
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