Flow modes during stabilization of the flutter of turbocompressor rotor blades

DOI10.1134/S1028335813020079zbMath1299.70040OpenAlexW2075111110MaRDI QIDQ5413005

R. F. Ganiev, O. B. Balakshin, B. G. Kukharenko

Publication date: 28 April 2014

Published in: Doklady Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1028335813020079

zbMATH Keywords

flutterProny methodbladesflutter spectral parametersturbocompressor rotor

Mathematics Subject Classification ID

General theory of rotating fluids (76U05) Modal analysis in linear vibration theory (70J10)

Cites Work

• Bifurcation of resonance during flutter of the blades of a turbocompressor rotor
• Stall flutter for incomplete synchronization of turbocompressor-blade vibrations

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