Behavior of curved laminated composite panels and shells under axial compression

H. Abramovich; C. Bisagni

doi:10.1016/j.paerosci.2015.05.008

Behavior of curved laminated composite panels and shells under axial compression

Research output: Contribution to journal › Review article › peer-review

Abstract

The buckling and post-buckling behavior of curved cylindrical stringer-stiffened laminated composite and metal panels had been investigated both numerically and experimentally. The results were compared to those of cylindrical stringer-stiffened laminated composite shells to yield a way of determining the optimal structure to be used for axial compression loading. For the present tested structures, the composite panels showed the best load-weight ratio.

Original language	English
Pages (from-to)	74-106
Number of pages	33
Journal	Progress in Aerospace Sciences
Volume	78
DOIs	https://doi.org/10.1016/j.paerosci.2015.05.008
State	Published - Oct 2015

Keywords

Buckling tests
Curved cylindrical panels
Shell structures
Post-buckling behavior
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ASJC Scopus subject areas

Aerospace Engineering
Mechanics of Materials
Mechanical Engineering

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10.1016/j.paerosci.2015.05.008

Cite this

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title = "Behavior of curved laminated composite panels and shells under axial compression",

abstract = "The buckling and post-buckling behavior of curved cylindrical stringer-stiffened laminated composite and metal panels had been investigated both numerically and experimentally. The results were compared to those of cylindrical stringer-stiffened laminated composite shells to yield a way of determining the optimal structure to be used for axial compression loading. For the present tested structures, the composite panels showed the best load-weight ratio.",

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author = "H. Abramovich and C. Bisagni",

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KW - Buckling tests

KW - Curved cylindrical panels

KW - Shell structures

KW - Post-buckling behavior

KW - Collapse

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JO - Progress in Aerospace Sciences

JF - Progress in Aerospace Sciences

ER -

Behavior of curved laminated composite panels and shells under axial compression

Abstract

Keywords

ASJC Scopus subject areas

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