Influence of Fibre Orientation on the Dynamic Behaviour of Rotating Laminated Composite Blades

DOI<link itemprop=identifier href="https://doi.org/10.1002/(SICI)1099-0887(199710)13:10<815::AID-CNM110>3.0.CO;2-W" /><815::AID-CNM110>3.0.CO;2-W 10.1002/(SICI)1099-0887(199710)13:10<815::AID-CNM110>3.0.CO;2-WzbMath0889.73040OpenAlexW2063790822MaRDI QIDQ4363344

Georges Jacquet-Richardet, Pascal Swider

Publication date: 18 June 1998

Full work available at URL: https://doi.org/10.1002/(sici)1099-0887(199710)13:10<815::aid-cnm110>3.0.co;2-w

zbMATH Keywords

mode shapesnatural frequenciesstructural dampinggeometrically nonlinear analysisautomatic tailoring techniquesmultilayered degenerated-solid shell elements

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)

Related Items (1)

Finite element linear and nonlinear, static and dynamic analysis of structural elements – an addendum – A bibliography (1996‐1999)

Cites Work

• Unnamed Item
• Aeroelastic tailoring analysis for advanced turbo propellers with composite blades
• Free vibration behavior of spinning shear-deformable plates composedof composite materials
• Analysis of laminated composite shells using a degenerated 3-D element
• Explicit thickness integration for three‐dimensional shell elements applied to non‐linear analysis

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