On the influence of laminate stacking on buckling of composite cylindrical shells subjected to axial compresssion
Geier, B. and Meyer-Piening, H.-R. and Zimmermann, R. (2002) On the influence of laminate stacking on buckling of composite cylindrical shells subjected to axial compresssion. Composite Structures, 55 (4), pp. 467-474.
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The buckling loads of laminated cylinders can strongly depend on the position of the differently oriented layers within the shell. This paper deals with two different laminated orthotropic cylinders with opposite stacking sequence of the laminate layers. Cylinders of this construction had been thoroughly tested within a BRITE EURAM project. Analytical and semi-analytical methods have been used to predict the buckling loads, and the results are reported in this paper as well as test results for comparison. An explanation of the striking influence of stacking sequence is given. With some more examples the findings are verified. It is suggested that the presented results can be used for benchmarking purpose.
|Title:||On the influence of laminate stacking on buckling of composite cylindrical shells subjected to axial compresssion|
|Journal or Publication Title:||Composite Structures|
|In ISI Web of Science:||Yes|
|Page Range:||pp. 467-474|
|Keywords:||Composites; Buckling analysis; Shells|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L - no assignement|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L ST - Starrflüglertechnologien|
|DLR - Research theme (Project):||UNSPECIFIED|
|Institutes and Institutions:||Institute of Composite Structures and Adaptive Systems > Institut für Strukturmechanik|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||16 Sep 2005|
|Last Modified:||14 Jan 2010 16:20|
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