Collapse characteristics of cylindrical composite panels under axial loads

The non-linear static response of a laminated graphite/epoxy cylindrical shell was investigated while subjected to an axially distributed load with cutout positioning. A 36 degrees-of-freedom two-dimensional curved rectangular finite element was incorporated into the through-the-thickness transverse...

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Bibliographische Detailangaben

Veröffentlicht in:	AIAA journal 1992-05, Vol.30 (5), p.1447-1449
Hauptverfasser:	SCHIMMELS, S. A, PALAZOTTO, A. N
Format:	Artikel
Sprache:	eng
Schlagworte:	Buckling Exact sciences and technology Fundamental areas of phenomenology (including applications) Physics Solid mechanics Structural and continuum mechanics
Online-Zugang:	Volltext
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