Stability analysis of nonlinear vibrations of a deploying flexible beam

DOI10.1016/S1007-5704(96)90050-7zbMath0922.73019OpenAlexW2038828438MaRDI QIDQ1289734

Zhao-Lin Wang, Jun-Feng Li

Publication date: 17 June 1999

Published in: Communications in Nonlinear Science and Numerical Simulation (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s1007-5704(96)90050-7

zbMATH Keywords

Lyapunov functionenergy integralflexible appendagefinite deflection beamlinear constitutive equationpartial stability theorem

Mathematics Subject Classification ID

Rods (beams, columns, shafts, arches, rings, etc.) (74K10) Vibrations in dynamical problems in solid mechanics (74H45) Stability of dynamical problems in solid mechanics (74H55)

Cites Work

• A general formulation for librational dynamics of spacecraft with deploying appendages

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