Buckling and vibration of finite-length composite prismatic plate structures with diaphragm ends. I: Finite strip formulation

DOI10.1016/0045-7825(89)90126-6zbMath0709.73029OpenAlexW1965009375MaRDI QIDQ922032

D. J. Dawe, V. Peshkam

Publication date: 1989

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7825(89)90126-6

zbMATH Keywords

eigenvaluesextended Sturm sequence-bisection approachgeometric stiffness matrixfibre-reinforced composite materiallaminatesconsistent mass matrixfirst-order shear deformation plate theorybending/stretching couplingclassical plate theoryelastic stiffness matrixfinite series of products of longitudinal trigonometric functions and crosswise polynomial functionsfinite strip method is of the multi-term typein-plane shear stressnatural frequencies of vibrationout-of-plane propertiespotential energy principlesStrip propertiessubstructuring schemesuperstrips

Mathematics Subject Classification ID

Anisotropy in solid mechanics (74E10) Vibrations in dynamical problems in solid mechanics (74H45) Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Bifurcation and buckling (74G60)

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