Buckling optimization of laminated cylindrical panels subjected to axial compressive load

Hsuan Teh Hu; Jiing Sen Yang

doi:10.1016/j.compstruct.2006.08.025

Buckling optimization of laminated cylindrical panels subjected to axial compressive load

Hsuan Teh Hu, Jiing Sen Yang

Department of Civil Engineering

Research output: Contribution to journal › Article › peer-review

28 Citations (Scopus)

Abstract

The buckling resistance of fiber-reinforced laminated cylindrical panels with a given material system and subjected to uniaxial compressive force is maximized with respect to fiber orientations by using a sequential linear programming method together with a simple move-limit strategy. The significant influences of panel thicknesses, curvatures, aspect ratios, cutouts and end conditions on the optimal fiber orientations and the associated optimal buckling loads of laminated cylindrical panels have been shown through this investigation.

Original language	English
Pages (from-to)	374-385
Number of pages	12
Journal	Composite Structures
Volume	81
Issue number	3
DOIs	https://doi.org/10.1016/j.compstruct.2006.08.025
Publication status	Published - 2007 Dec

All Science Journal Classification (ASJC) codes

Ceramics and Composites
Civil and Structural Engineering

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10.1016/j.compstruct.2006.08.025

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abstract = "The buckling resistance of fiber-reinforced laminated cylindrical panels with a given material system and subjected to uniaxial compressive force is maximized with respect to fiber orientations by using a sequential linear programming method together with a simple move-limit strategy. The significant influences of panel thicknesses, curvatures, aspect ratios, cutouts and end conditions on the optimal fiber orientations and the associated optimal buckling loads of laminated cylindrical panels have been shown through this investigation.",

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AB - The buckling resistance of fiber-reinforced laminated cylindrical panels with a given material system and subjected to uniaxial compressive force is maximized with respect to fiber orientations by using a sequential linear programming method together with a simple move-limit strategy. The significant influences of panel thicknesses, curvatures, aspect ratios, cutouts and end conditions on the optimal fiber orientations and the associated optimal buckling loads of laminated cylindrical panels have been shown through this investigation.

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Buckling optimization of laminated cylindrical panels subjected to axial compressive load

Abstract

All Science Journal Classification (ASJC) codes

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