Dynamic instability of spinning launch vehicles modeled as thin-walled composite beams

DOI10.1007/S00707-017-1944-YzbMath1380.74055OpenAlexW2747733069MaRDI QIDQ1696161

Seher Eken, Melahat Cihan, Metin Orhan Kaya

Publication date: 14 February 2018

Published in: Acta Mechanica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00707-017-1944-y

Mathematics Subject Classification ID

Rods (beams, columns, shafts, arches, rings, etc.) (74K10) Stability of dynamical problems in solid mechanics (74H55) Random materials and composite materials (74A40)

Related Items (2)

Effects of residual stress and viscous and hysteretic dampings on the stability of a spinning micro-shaft ⋮ Dynamic stability of fluid-conveying thin-walled rotating pipes reinforced with functionally graded carbon nanotubes

Cites Work

• Transfer matrix method for the determination of the natural vibration characteristics of realistic thrusting launch vehicle -- part I
• Thin-walled composite beams. Theory and application
• Missile stability using finite elements - An unconstrained variational approach

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