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a study of parametric resonance in the u0430u0432u0442u043eu043au043eu043bu0435u0431u0430u043du0438u044fu0445 on u043au0440u0435u043du0443 aerodynamic models
a study of parametric resonance in the u0430u0432u0442u043eu043au043eu043bu0435u0431u0430u043du0438u044fu0445 on u043au0440u0435u043du0443 aerodynamic models
a study of parametric resonance in the u0430u0432u0442u043eu043au043eu043bu0435u0431u0430u043du0438u00a0u0445 on u043au0440u0435u043du0443 aerodynamic models, including the model in the flow of a wind pipe s, finding her at the angle of attack in which the u0432u043eu0437u0431u0443u0436u0434u0430u044eu0442u0441u00a0 u0430u0432u0442u043eu043au043eu043bu0435u0431u0430u043du0438u00a0 and changing their parameters, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 whatin order to u043fu043eu0432u044bu0448u0435u043du0438u00a0 accuracy u043cu043eu0434u0435u043bu0438u0440u043eu0432u0430u043du0438u00a0 real flight conditions of an aircraft by u0437u0430u0434u0430u043du0438u00a0 parametric perturbations on the angle of attack, after the withdrawal of mo new delhi at the angle of attack are oscillatory u043fu0435u0440u0435u043cu0435u0449u0435u043du0438u00a0 it vertically, with a continuously u0438u0437u043cu0435u043du00a0u044eu0449u0435u0439u0441u00a0 u0438u0437u043cu0435u0440u00a0u044eu0442 frequency and frequency of these movements.
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