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Meccanica
Erschienen in: Meccanica 4/2016

23.07.2015

Dynamic instability of parabolic shells in supersonic gas stream

verfasst von: K. V. Avramov, M. V. Chernobryvko, O. Kazachenko, T. J. Batutina

Erschienen in: Meccanica | Ausgabe 4/2016

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Abstract

The dynamic instability of the parabolic shells in a supersonic gas flow is analyzed numerically. Such structures describe a rocket fairing. Finite degrees of freedom dynamical system is obtained by the assumed-modes method to describe the shell motions. The numerical approach for calculations the modes of the shell self-sustained vibrations is suggested. The Mach numbers range of the shell dynamic instability is analyzed numerically. The influence of the paraboloid height on the regions of the dynamic instability is analyzed. The frequencies of the self-sustained vibrations are investigated. The effect of the shell boundary conditions on the regions of the dynamic instability is analyzed.
Vorheriger Artikel Three dimensional static and free vibration analysis of cross-ply laminated plate bonded with piezoelectric layers using differential quadrature method
Nächster Artikel In-plane thermal loading effects on vibrational characteristics of functionally graded nanobeams

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Metadaten
Titel
Dynamic instability of parabolic shells in supersonic gas stream
verfasst von
K. V. Avramov
M. V. Chernobryvko
O. Kazachenko
T. J. Batutina
Publikationsdatum
23.07.2015
Verlag
Springer Netherlands
Erschienen in
Meccanica / Ausgabe 4/2016
Print ISSN: 0025-6455
Elektronische ISSN: 1572-9648
DOI
https://doi.org/10.1007/s11012-015-0247-4

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