On the stability of a flexible missile under an end thrust

DOI10.1016/0895-7177(90)90322-EzbMath0729.73084OpenAlexW1967544730MaRDI QIDQ807131

K. Ossia, Ardéshir Guran

Publication date: 1990

Published in: Mathematical and Computer Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0895-7177(90)90322-e

zbMATH Keywords

eigenvaluesHopf bifurcationflutternon-self-adjoint operatorconvergence characteristicseigenvalue curvesconcept of transfer matrixcritical thrustline-search problemuniform free-free rod

Mathematics Subject Classification ID

Stability of dynamical problems in solid mechanics (74H55) Finite difference methods applied to problems in solid mechanics (74S20)

Related Items (1)

Stability of a flexible missile and asymptotics of the eigenvalues of fourth order boundary value problems

Cites Work

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• Finite element method applied to the problem of stability of a non‐conservative system

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