Free vibration and buckling response of hat-stiffened composite panels under general loading

DOI10.1016/J.IJMECSCI.2008.03.003zbMath1264.74097OpenAlexW2055337061MaRDI QIDQ1953617

B. Gangadhara Prusty

Publication date: 7 June 2013

Published in: International Journal of Mechanical Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ijmecsci.2008.03.003

zbMATH Keywords

bucklingshellfree vibrationstiffenedlaminated composites

Mathematics Subject Classification ID

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) Shells (74K25)

Related Items (4)

Buckling analysis of stringer-stiffened laminated cylindrical shells with nonuniform eccentricity ⋮ A genetic algorithm optimization of ring-stiffened cylindrical shells for axial and radial buckling loads ⋮ Dynamic near three-to-one internal resonance in composite stiffened panels ⋮ A numerical approach for limit analysis of orthotropic composite laminates

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